TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Kossira, H. T1 - Beschreibung des intralaminaren Ermüdungsverhaltens von Faserverbundwerkstoffen T2 - DGLR-Jahrestagung 2001 CY - Hamburg, Germany DA - 2001-09-17 PY - 2001 AN - OPUS4-3396 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Zerstörungsfreie Charakterisierung des Schädigungszustandes von CFK infolge intralaminarer Ermüdungsbeanspruchung T2 - Jahrestagung Zerstörungsfreie Materialprüfung 2001 CY - Berlin, Deutschland DA - 2001-05-21 PY - 2001 UR - http://www.ndt.net/article/dgzfp01/papers/v39/v39.htm N1 - Serientitel: Berichtsband / Deutsche Gesellschaft für zerstörungsfreie Prüfung e. V. – Series title: Berichtsband / Deutsche Gesellschaft für zerstörungsfreie Prüfung e. V. IS - 75-CD PB - DGZfP CY - Berlin AN - OPUS4-1875 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Kossira, H. T1 - Charakterisierung der intralaminaren Werkstoffermüdung von CFK PY - 2002 SN - 0025-5300 VL - 44 IS - 1-2 SP - 6 EP - 12 PB - Carl Hanser Verlag CY - München AN - OPUS4-1876 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kossira, H. A1 - Harbich, Karl-Wolfram T1 - Beschreibung des intralaminaren Ermüdungsverhaltens von Faserverbundwerkstoffen T2 - Deutscher Luft- und Raumfahrtkongress 2001 CY - Hamburg, Deutschland DA - 2001-09-17 PY - 2001 SN - 0070-4083 SP - 1(?) EP - 10(?) PB - DGLR CY - Bonn AN - OPUS4-1877 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy T1 - Intralaminar Fatigue Behaviour of CFRP T2 - European Conference on Spacecraft Structures Materials and Mechanical Testing CY - Toulouse, France DA - 2002-12-11 PY - 2002 AN - OPUS4-1878 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Harbich, Karl-Wolfram A1 - Hentschel, Manfred P. A1 - Ivers, Heinz A1 - Rudolph, Hans-Volker A1 - Trappe, Volker A1 - Niebergall, Ute T1 - Mikroriss-Charakterisierung mittels Röntgen-Refraktions-Topographie N2 - Einleitung Bei der Detektion von Mikrorissen und der Charakterisierung spezifischer Schädigungen von Polymer- und Kompositwerkstoffen kommt es neben quantitativen Bewertungen auch auf die Analyse von orientierungsabhängigen Struktureffekten an. Am Beispiel typischer Vertreter ausgewählter Materialien (PP/PE, CFK) wird dargestellt, inwieweit das Potential der Röntgen-Refraktions-Topographie vorteilhaft zur umfassenden Materialcharakterisierung genutzt werden kann. Die korrosiven Eigenschaften nichtmetallischer Werkstoffe werden maßgeblich vom mikrostrukturellen Aufbau der verwendeten Materialien bestimmt. Typische Versagens-mechanismen von Faser-Kompositen sind neben der Faserenthaftung vor allem durch Mikrorisse gekennzeichnet, die sich teils parallel, teils senkrecht zu den Fasern in der Matrix ausbreiten. Eine wichtige Anwendung der Röntgen-Refraktions-Topographie umfaßt die orientierungsselektive Detektion von Mikroriß-Oberflächen. Die Nachweisgrenze derartiger Schädigungen erstreckt sich bis zum Nanometerbereich. Definiert herbeigeführte Ermüdungsschäden an Kompositmaterialien lassen sich mit dieser Methode ausgezeichnet erfassen und gestatten eine quantitative Korrelation zu mechanischen Kenngrößen. Mittels schrittweiser Probenabtastung und der ortskorrelierten Speicherung von simultan erfassten Refraktions- bzw. Absorptionszählraten wird ein zweidimensionales Röntgen-Refraktions-Topogramm rekonstruiert, das u.a. die präzise Information der integralen Rissdichte enthält. T2 - Jahrestagung Zerstörungsfreie Materialprüfung 2002 CY - Weimar, Deutschland DA - 2002-05-06 PY - 2002 UR - http://www.ndt.net/article/dgzfp02/papers/p18/p18.htm SN - 3-931381-39-0 N1 - Serientitel: Berichtsband / Deutsche Gesellschaft für zerstörungsfreie Prüfung e. V. – Series title: Berichtsband / Deutsche Gesellschaft für zerstörungsfreie Prüfung e. V. IS - 80-CD PB - DGZfP CY - Berlin AN - OPUS4-1879 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy T1 - Damage State of Characterized Non-Destructively by X-Ray-Refraction-Topography and Ultrasound T2 - SAMPE-Tagung 2003 CY - Long Beach, CA, USA DA - 2003-05-11 PY - 2003 AN - OPUS4-2908 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy ED - Green, R. E. ED - Djordjevic, B. B. ED - Hentschel, M. P. T1 - Micro cracking and stress state under fatigue loading of CFRP T2 - 11th International Symposium on Nondestructive Characterization of Materials CY - Berlin, Germany DA - 2002-06-24 PY - 2003 SN - 3-540-40154-7 SP - 697 EP - 704 PB - Springer CY - Berlin AN - OPUS4-2770 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy T1 - Micro Cracking and Stress State under Fatigue Loading of CFRP T2 - 11th International Symposium on Non-destructive Charakterization of Materials (CNDE) CY - Berlin, Germany DA - 2002-06-24 PY - 2002 AN - OPUS4-7444 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy T1 - Intralaminar Fatigue Behaviour of CFRP T2 - European Conference on Spacecraft Structures Materials & Mechanical Testing CY - Toulouse, France DA - 2002-12-11 PY - 2002 AN - OPUS4-7441 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram T1 - Description of the Micro Cracking of CFRP under Matrix Dominated Fatigue Loading T2 - 16. Workshop "Composite Forschung in der Mechanik" CY - Paderborn, Germany DA - 2003-12-01 PY - 2003 AN - OPUS4-4101 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram A1 - Ernst, Hardy T1 - Damage state of CFRP characterized non-destructively by X-ray-refraction-topography and ultrasound T2 - 48th International SAMPE Symposium CY - Long Beach, CA, USA DA - 2003-05-10 PY - 2003 AN - OPUS4-4102 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Charakterisierung des Schädigungszustandes von FVW unter Betriebsbeanspruchung T2 - 27. Segelflugsymposium CY - Braunschweig, Germany DA - 2003-11-20 PY - 2003 AN - OPUS4-4103 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hentschel, Manfred P. T1 - Non-invasive characterisation of intra laminar fatique of carbon fibre composites Aero NDT Forum T2 - Aerospace Testing EXPO 2004 CY - Hamburg, Germany DA - 2004-03-30 PY - 2004 AN - OPUS4-5577 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hentschel, Manfred P. A1 - Ivers, Heinz T1 - Micro-mechanical properties of fiber composites characterized by X-ray refraction T2 - SPIE NDE-Symposium 2005 CY - San Diego, CA, USA DA - 2005-03-06 PY - 2005 AN - OPUS4-7061 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hentschel, Manfred P. A1 - Ivers, Heinz T1 - Bestimmung des Zwischenfaserbruchversagens in komplexen, textilen Faserverbundwerkstoffen T2 - Deutscher Luft- und Raumfahrtkongress CY - Friedrichshafen, Germany DA - 2005-09-27 PY - 2005 AN - OPUS4-11382 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Achelpöhler-Schulte, Andreas A1 - Ell, Matthias T1 - Ergebnisse der Untersuchungen an Proben und Holmen zur Zulassung von HTS-Kohlenstofffasern für die Segelflugzeugindustrie T2 - Symposium Segelflugzeugentwicklung CY - Braunschweig, Germany DA - 2005-11-17 PY - 2005 AN - OPUS4-11383 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Kleben von Faserverbundwerkstoffen T2 - Polymerwissenschaftliches Seminar an der TU-Berlin CY - Berlin, Germany DA - 2005-10-25 PY - 2005 AN - OPUS4-11384 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hentschel, Manfred P. A1 - Ivers, Heinz T1 - Zerstörungsfreie Bestimmung des Zwischenfaserbruchversagens in Faserverbundwerkstoffen mit Hilfe der Röntgenrefraktionstopographie T2 - DVM-Tagung Werkstoffprüfung 2005 CY - Berlin, Germany DA - 2005-12-01 PY - 2005 AN - OPUS4-11385 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Life cycle of FRP-components due to in-service loading T2 - Aerospace Testing, Expo 2005 CY - Hamburg, Germany DA - 2005-04-06 PY - 2005 AN - OPUS4-11386 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Life cycle of FRP-components due to in-service loading T2 - Branchenkonferenz der Luft- und Raumfahrt CY - Cottbus, Germany DA - 2005-09-06 PY - 2005 AN - OPUS4-11387 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Determination of inter-fibre-failure in complex, reinforced composites T2 - Aerospace Testing Expo 2005 CY - Hamburg, Germany DA - 2005-04-06 PY - 2005 AN - OPUS4-11388 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Hörold, Andreas A1 - Schartel, Bernhard A1 - Trappe, Volker A1 - Korzen, Manfred A1 - Naumann, Maurice T1 - Structural integrity in fire: an intermediate-scale approach T2 - ECCM15 - 15th European conference on composite materials CY - Venice, Italy DA - 2012-06-24 KW - Intermediate-scale test method KW - Structural integrity investigation KW - Fully developed fire KW - Carbon fibre reinforced plastics CFRP PY - 2012 SN - 978-88-88785-33-2 SP - 1 EP - 8(?) AN - OPUS4-26380 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Jaunich, Matthias ED - Yao, W. ED - Renard, J. ED - Himmel, N.A. T1 - Correlation between crack propagation rate and cure process of epoxy resins KW - Fracture toughness KW - Crack resistance KW - Fracture mechanics KW - Plastics KW - Crack propagation PY - 2012 SN - 978-1-60595-091-4 SP - 277 EP - 290 PB - DEStech Publications, Inc. CY - Lancaster, PA, USA AN - OPUS4-27947 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebsfestigkeit und Zustandsüberwachung von Rotorblättern - Verifikation über Stellvertreterversuche T2 - Vortrag auf Tagung "Spree-WIND 2011" CY - Schönefeld, Germany DA - 2011-10-25 PY - 2011 AN - OPUS4-24681 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Grasse, Fabian A1 - Trappe, Volker A1 - Thöns, Sebastian A1 - Said, Samir ED - De Roeck, G. ED - Degrande, G. ED - Lombaert, G. ED - Müller, G. T1 - Structural health monitoring of wind turbine blades by strain measurement and vibration analysis N2 - Wind turbine blades have to withstand a high number of load cycles in mostly hard weather conditions over 20 years. In a research project BAM and several partners have designed, evaluated and tested a condition monitoring system for all parts of a wind turbine. At a rotorblade with a length of 58 m fibre bragg grating sensors were applied for in-service strain measurement. Additionally a complex test rig was designed to enable real biaxial loading conditions at a representative test rotor blade to simulate the mechanical loading conditions in the lab. In this test blade with a length of 8 m also fibre bragg grating sensors were implemented to determine their influences for the structure and the condition monitoring system. Vibration measurements were carried out at different test phases. The results were compared with finite element strain and modal analysis. T2 - EURODYN 2011 - 8th International conference on structural dynamics CY - Leuven, Belgium DA - 04.07.2011 KW - Rotor blade KW - Test blade KW - Modal analysis KW - Condition monitoring PY - 2011 SN - 978-90-760-1931-4 IS - MS25 Tue SP - 3490 EP - 3497 AN - OPUS4-25076 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Grasse, Fabian A1 - Trappe, Volker A1 - Hickmann, Stefan ED - Grellmann, W. T1 - Zustandsüberwachung von Rotorblättern - Konzeptstudie mittels Bauteilkomponentenversuch T2 - DVM-Tagung Werkstoffprüfung 2011 - Neue Entwicklungen in der Werkstoffprüfung - Herausforderungen an die Kennwertermittlung CY - Berlin, Deutschland DA - 2011-12-01 KW - Rotorblatt KW - Faserverbundwerkstoffe KW - Modalanalyse KW - Zustandsüberwachung KW - Faser-Bragg-Gitter-Sensoren KW - Rotor blade KW - Fibre reinforced plastics KW - Modal analysis KW - Condition monitoring KW - Fibre bragg grating sensors PY - 2011 SN - 978-3-9814516-1-0 SN - 1861-8154 N1 - Serientitel: DVM-Bericht – Series title: DVM-Bericht IS - 643 SP - 167 EP - 172 AN - OPUS4-25078 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Grasse, Fabian A1 - Thöns, Sebastian A1 - Said, Samir T1 - Structural health monitoring for wind turbine rotor blades by strain measurement and vibration T2 - EURODYN 2011 CY - Leuven, Belgium DA - 2011-07-04 PY - 2011 AN - OPUS4-25093 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Praxisgerechte und effiziente Prüfung der Betriebsfestigkeit von Faserverbundwerkstoffen und -bauteilen T2 - TU Hamburg-Harburg, Einladung zum Institutsseminar des Institute of Polymers and Composites, Prof. Schulte CY - Hamburg, Germany DA - 2011-02-24 PY - 2011 AN - OPUS4-25095 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Ortwein, Hans-Peter A1 - Bohse, Jürgen A1 - Trappe, Volker A1 - Hickmann, Stefan T1 - Untersuchung des Zwischenfaserrisswachstums in Faserverbundwerkstoffen mit Schallemissions- und Röntgenrefraktionsverfahren N2 - Hinsichtlich Materialermüdung und Betriebsfestigkeit in Faserkunststoffverbunden besteht - verglichen mit anderen Aspekten des Faserverbundleichtbaues – noch erheblicher Forschungsbedarf. Schon weit vor den globalen Festigkeiten des Laminates treten eine Vielzahl von Zwischenfaserbrüchen und vereinzelte Faserbrüche auf. Die Dichte dieser Mikrorisse soll hier als Indikator für den Zustand des Verbundes genutzt werden. Ihre Ermittlung stellt insbesondere bei Kohlenstofffasern eine Herausforderung dar. Über vergleichende Messungen mit der Schallemissionsanalyse (SEA) und der Röntgenrefraktionsscans (RR) wird die Entwicklung der Rissdichte bei Belastung untersucht. Die SEA zeichnet die Entstehung der Risse auf und kann wegen der kompakten Messtechnik auch gut am Bauteil eingesetzt werden. Die RR beobachtet die Änderung der inneren Grenzflächen, die ebenfalls die Entwicklung der Rissdichte widerspiegelt. Sie ist allerdings zurzeit nur als Laborverfahren geeignet. Der Vortrag berichtet(e) über den aktuellen Stand des vergleichenden Einsatzes beider Verfahren an Flachproben und innendruckbelasteten Rohrproben. T2 - DGZfP-Jahrestagung 2011 CY - Bremen, Deutschland DA - 30.05.2011 KW - Schallemissionsprüfung KW - Röntgenrefraktionsmessung KW - Faserkunstoffverbund KW - Druckbehälter PY - 2011 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-248913 SN - 978-3-940283-33-7 SP - Mi.4.A.1 - 1 EP - 8 PB - Deutsche Gesellschaft für Zerstörungsfreie Prüfung (DGZfP) AN - OPUS4-24891 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Ortwein, Hans-Peter A1 - Bohse, Jürgen A1 - Trappe, Volker T1 - Untersuchung der Mikrorissbildung in Faserkunststoffverbunden mittels Röntgenrefraktions- und Schallemissionsmessung N2 - Hinsichtlich Materialermüdung in Faserkunststoffverbunden besteht verglichen mit anderen Aspekten des Faserverbundleichtbaues – noch erheblicher Forschungsbedarf. Schon weit vor den globalen Festigkeiten des Laminates treten eine Vielzahl von Zwischenfaserbrüchen und vereinzelte Faserbrüche auf. Die Dichte dieser Mikrorisse soll als Indikator für den Zustand des Verbundes genutzt werden. Ihre Ermittlung stellt insbesondere bei Kohlenstofffasern eine Herausforderung dar. Über vergleichende Messungen mit der Schallemissionsanalyse (SEA) und der Röntgenrefraktionsanalyse (RR) wird die Entwicklung der Rissdichte bei Belastung untersucht. die SEA zeichnet die Entstehung der Risse auf und kann wegen der kompakten Messtechnik auch gut am Bauteil eingesetzt werden Die RR beobachtet die Änderung der inneren Grenzflächen, die ebenfalls eine Entwicklung der Rissdichte widerspiegelt. Sie ist allerdings zurzeit nur als Laborverfahren geeignet. Der Vortrag berichtet über den aktuellen Stand des vergleichenden Einsatzes beider Verfahren an Zugproben und Modellbehältern. T2 - 18. Kolloquium Schallemission CY - Wetzlar, Deutschland DA - 27.10.2011 KW - Schallemissionsprüfung KW - Röntgenrefraktionsmessung KW - Faserkunststoffverbund KW - Druckbehälter PY - 2011 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-248926 SN - 978-3-940283-37-5 VL - 131 SP - V05-1 EP - 7 AN - OPUS4-24892 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Ortwein, Hans-Peter A1 - Trappe, Volker A1 - Bohse, Jürgen A1 - Hickmann, Stefan ED - Grellmann, W. T1 - In-Situ-Messung der Matrixschädigung in kohlenstofffaserverstärktem Kunststoff unter uni- und biaxialer Zugbelastung N2 - Die Restlebensdauerabschätzung von Faserkunststoffverbunden ist ein ungelöstes Problem. Die Beobachtung der Matrixschädigung ist dabei ein vielversprechender Ansatz zur Bewertung des Schädigungszustandes insgesamt. Unter kombinierter Beobachtung mit Röntgenrefraktionsmessungen und Schallemissionsmessung wurden uni- und biaxiale Lasten statisch und zyklisch auf Kohlenstofffaserepoxidharz-Proben aufgebracht. Die uniaxiale Belastung erfolgt mittels einer eigenentwickelten Kompaktprüfmaschine direkt während der Röntgenrefraktions- und Schallemissionsmessung in der Röntgenkammer. Die biaxiale Belastung wird an Modelldruckbehältern ebenfalls mit Schallemissionsmessung durchgeführt. Hier wird der Modelldruckbehälter mit dem Röntgenrefraktionsverfahren periodisch inspiziert. T2 - DVM-Tagung Werkstoffprüfung 2011 - Neue Entwicklungen in der Werkstoffprüfung - Herausforderungen an die Kennwertermittlung CY - Berlin, Germany DA - 01.12.2011 KW - Druckbehälterprüfung KW - CFK KW - Schallemissionsmessung KW - Röntgenrefraktionsmessung KW - Matrixschädigung KW - Faserkunststoffverbund KW - Druckbehälter PY - 2011 SN - 978-3-9814516-1-0 SN - 1861-8154 N1 - Serientitel: DVM-Bericht – Series title: DVM-Bericht IS - 643 SP - 161 EP - 166 AN - OPUS4-24931 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebszeitfeste Auslegung von FVK - Effekte, Grenzen, Möglichkeiten T2 - IKV-Fachtagung zur Kunststoffverarbeitung CY - Aachen, Germany DA - 2011-11-24 PY - 2011 AN - OPUS4-24846 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebsfestigkeitsnachweis für Segelflugzeuge aus FKV - Konzepte, Historie, Entwicklungen T2 - 35. Symposium für Segelflugzeugentwicklung, Wasserkuppe (Rhön) CY - Fulda, Germany DA - 2011-11-17 PY - 2011 AN - OPUS4-24847 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Goebbels, Jürgen T1 - Zerstörungsfreie Charakterisierung des Schädigungszustandes von Kurzglasfaserverstärkten Thermoplasten mit Röntgenverfahren T2 - DACH-Jahrestagung 2012 CY - Graz, Austria DA - 2012-09-17 KW - Kurzfaserverstärktes Polyamid KW - ZfP mit Röntgenverfahren KW - Mikrorissbildung KW - Schädigungsverhalten PY - 2012 SN - 978-3-940283-44-3 IS - DGZfP-BB 136 SP - Mo.3.C.4., 1 EP - 6 AN - OPUS4-27704 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Zerstörungsfreie Prüfung von Faser-Kunststoff-Verbunden (FKV) - Korrelation mit Festigkeit und Ermüdung am Beispiel von Röntgenverfahren T2 - CCeV-Thementag Ermüdung von FKV CY - Augsburg, Germany DA - 2013-02-14 PY - 2013 AN - OPUS4-27713 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Advanced composite testing to assure high quality and blade performance T2 - Advances in wind turbine rotor blades CY - Bremen, Germany DA - 2012-02-13 PY - 2012 AN - OPUS4-25570 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Hörold, Andreas A1 - Schartel, Bernhard A1 - Trappe, Volker A1 - Korzen, Manfred T1 - An intermediate-scale fire testing approach on the structural integrity of lightweight materials N2 - Carbon or glass über composites and Sandwich structures, the lightweight materials of choice for aviation, naval, offshore and construction show an enormous energy saving potential. Their combination of excellent specific mechanical properties, high corrosive resistance and thermal insulation properties in combination with various adoptable fabrication techniques leading to mass and fuel cost reduction. The most limiting single factor for a wider use of fibre reinforced plastics (FRP) in particular as elements for structural application is believed to be their fire behaviour (Mouritz and Gibson, 2006). FRPs promote burning by themselves consuming the stabilizing polymeric matrix while embedded fibers (glass, carbon) persisting the flame (Mouritz et ah, 2006). Already at elevated temperatures (100 - 200 °C) the matrix softens with a loss in mechanical properties (Perret et al., 2011, Mouritz and Gibson, 2006). For this reason the stability of the structural component is decreased severely. Fire behavior becomes the major hazard to worry about, increasingly demanding targetoriented investigation, suitable testing and tailored development. Experimental approaches in the bench-scale have been proposed to investigate the structural integrity in the past (La Delfa et al., 2009, Gibson et al., 2010, Seggewiß, 2011, Mouritz and Gardiner, 2002, Schartel et al.). Ascribed to the small-scale neither the mechanical properties nor the effects of fire may be represented satisfactorily. Flence, the task is to perform more realistic investigations under adequate compressive loads in fully developed fires, based on suitable specimen sizes. Also (La Delfa et al., 2009)) have announced that it is evident that larger scale test of composites are needed. The aim of this study is to present a developed intermediate-scale test setup to perform more realistic investigations (Hörold et al.). Mechanical loading is generated by a column furnace in terms of compression due to a more severe response of specimens in fire tests (Seggewiß, 2011, Gibson et al., 2012, Feih et al., 2008, Feih et al., 2007). An oil burner used to determine the burnthrough resistance of thermal/acoustic insulation materials provides fire directly onto one side of the specimen (Federal Aviation Administration, 2003). Generating a fully developed fire the NexGen burner offers a homogenous heat flux of ~ 180 kW/m2. The intermediate-scale is addressed by specimen sizes either 500 x 500 mm or 1000 x 500 mm with a maximum thickness of 50 mm. The specimen attachment is realized by a compression device that was designed to apply the compressive loads, figure 1. The test setup for specimens with component like dimensions allows realistic investigations up to structural failure in absence and presence of fire load. A first test series was carried out with different levels of loading while the fire remained unchanged. Failure mechanisms, temperature distributions, diversity of FRPs regarding fiber, matrix, lay-up and core as well as flame retardant Systems are in the scope of investigation. T2 - Fire and materials 2013 - 13th International conference and exhibition CY - San Francisco, CA, USA DA - 28.01.2013 PY - 2013 SP - 221 EP - 226 PB - Interscience Communications CY - London, UK AN - OPUS4-27782 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Bohse, Jürgen A1 - Rudolph, Hans-Volker A1 - Marotzke, Christian T1 - Understanding the strength of composite structures through the analysis of materials failure in a micro-meter and micro-second scale T2 - Structural Composite Conference CY - Birmingham, AL, USA DA - 2006-02-08 PY - 2006 AN - OPUS4-16336 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Faserverbundwerkstoffe mit Polymermatrix - Forschungsaktivitäten an der BAM T2 - Kolloquium des Institutes für Luft- und Raumfahrt, Technische Universität Berlin CY - Berlin, Germany DA - 2006-04-28 PY - 2006 AN - OPUS4-16337 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hamann, Andreas A1 - Löwe, Peter T1 - Festigkeits- und Ermüdungsverhalten von Faserverbundwerkstoffen, betrachtet im µm- und µs-Maßstab T2 - DVM/DGZfP-Kolloquium CY - Berlin, Germany DA - 2006-06-06 PY - 2006 AN - OPUS4-16338 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hentschel, Manfred P. A1 - Ivers, Heinz T1 - Determination of inter-fibre-failure in complex, reinforced composites T2 - 16th European Conference of Fracture CY - Alexandroupoli, Greece DA - 2006-07-03 PY - 2006 AN - OPUS4-16339 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Marotzke, Christian A1 - Ivers, Heinz T1 - Understanding the strength and fatigue behaviour of fibre composites by the analysis of micro cracking effects T2 - 11th International Conference on Mechanics and Technology of Composite Materials CY - Sofia, Bulgaria DA - 2006-10-02 PY - 2006 AN - OPUS4-16340 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Zerstörungsfreie Werkstoffprüfung - Verfahrensentwicklung für Composites T2 - Materialica 2006 CY - Munich, Germany DA - 2006-10-12 PY - 2006 AN - OPUS4-16341 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Grasse, Fabian A1 - Günzel, Stephan T1 - Zustand und Festigkeit - Ergebnisse der Ermüdungsbeanspruchung eines Versuchsflügels stellvertretend für GFK-Segelflugzeuge T2 - Symposium für Segelflugzeugentwicklung CY - Darmstadt, Germany DA - 2006-11-24 PY - 2006 AN - OPUS4-16342 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Sturm, Heinz T1 - Bestimmung des Zwischenfaserbruchversagens in textilverstärktem Glasfaserkunststoff mittels der Röntgenrefrationstopografie N2 - Moderne Leichtbaustrukturen (Luftfahrt, Eisenbahn, Automotive) aus Faserverbundwerkstoffen (FVW) sind hohen mechanischen und klimatischen Beanspruchungen ausgesetzt. Aussagen über die Lebensdauer und Funktionssicherheit der FVW-Bauteile können eher aus Untersuchungen der mikromechanischen Eigenschaften gewonnen werden als aus der globalen Festigkeit. Die Röntgenrefraktionstopografie ist ein Verfahren zur zerstörungsfreien Bestimmung von inneren Oberflächen in Werkstoffen. Angewendet auf FVW lassen sich Aussagen über die Faserorientierungen, die Fertigungsqualität sowie über Faser-Matrix-Ablösungen und Matrixrisse infolge mechanischer Beanspruchung gewinnen. Nachfolgend wird ein neues Verfahren zur Bestimmung des Zwischenfaserbruchversagens am komplexen Laminat vorgestellt. Hierbei wird das Röntgenrefraktionsverfahren "online“ bei Zug-Belastung der Probe angewendet. KW - Zerstörungsfreie Prüfung KW - Röntgenstreuung KW - Faserverbundwerkstoffe KW - Mikrorissbildung KW - Glasfaserverstärkter Kunststoff PY - 2008 SN - 0025-5300 VL - 50 IS - 10 SP - 615 EP - 622 PB - Hanser CY - München AN - OPUS4-18282 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Testing of lightweight composite structures - from complex component setup to micro-mechanical analysis T2 - Einladung zur IIR-Konferenz "Composite & Lightweight Structures in Aircraft" CY - Hamburg, Germany DA - 2007-07-03 PY - 2007 AN - OPUS4-14910 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Goebbels, Jürgen T1 - Möglichkeiten und Grenzen der Röntgen-Computertomographie zur Schadensdetektion bei Segelflugzeugen T2 - Symposium für Segelflugzeugentwicklung 2008, Wasserkuppe (Rhön) CY - Fulda, Germany DA - 2008-11-20 PY - 2008 AN - OPUS4-18088 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - RHV (Richtlinien zur Führung des Nachweises für die Anerkennung von Harz-Faser-Verbundsystemen) und Normung - Industriestandards kontra Norm? T2 - Symposium für Segelflugzeugentwicklung 2008, Wasserkuppe (Rhön) CY - Fulda, Germany DA - 2008-11-20 PY - 2008 AN - OPUS4-18089 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Evaluation of the non-linear stress-strain behaviour of CFRP during fatigue testing with inner state variables T2 - 6th International conference on Low Cycle Fatigue (LCF) CY - Berlin, Germany DA - 2008-09-09 PY - 2008 AN - OPUS4-18090 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Praxisgerechte und effiziente Prüfung von Faserverbundwerkstoffen T2 - Tagung "Kunststoffe - Trends und neue Anwendungen" CY - Berlin, Germany DA - 2008-06-17 PY - 2008 AN - OPUS4-18091 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Praxisgerechte und effiziente Prüfung von Faserverbundwerkstoffen T2 - Werkstoff-Forum Verbundwerkstoffe CY - Hanover, Germany DA - 2008-04-22 PY - 2008 AN - OPUS4-18092 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram T1 - Description of the Micro Cracking of CFRP under Matrix Dominated Fatigue Loading T2 - Polydays 2002, TU Berlin CY - Berlin, Germany DA - 2002-09-30 PY - 2002 AN - OPUS4-7486 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker A1 - Harbich, Karl-Wolfram T1 - Intralaminar fatigue behaviour of carbon fibre reinforced plastics N2 - A new approach is discussed for characterizing the damage state of FRP with the appearance of micro cracking and its influence on the residual strength. For the quantitative analysis of micro cracking, X-ray refraction topography was used. Fatigue treatment of carbon fibre reinforced plastics (CFRP) laminates were performed to create defined damage states. With regard to real loading conditions of CFRP, studies on tube samples were performed to investigate two dimensional (tension–torsion) loads. A rheological material model was presented which described the increase of micro cracking in ±45° CFRP laminates with a continuum mechanical approach. The correlation between the results of the X-ray refraction topography, the damage parameter of the rheological model and the decrease of residual strength were shown. The inter fibre fracture surface of the investigated CFRP materials was determined with tension–torsion loaded tube specimens of 90°-laminate and a layer-wise strength analysis was done. Micro cracking occurs even at 50% inter-fibre fracture loading and can lead to a distinct strength reduction. The intralaminar fatigue effect itself seems to be an indication for the damage accumulation and the load history. KW - Carbon fibre reinforced plastics KW - Damage accumulation KW - Damage state of CFRP KW - Inter- and intralaminar fatigue KW - Non-destructive testing PY - 2006 U6 - https://doi.org/10.1016/j.ijfatigue.2006.02.037 SN - 0142-1123 VL - 28 IS - 10 SP - 1187 EP - 1196 PB - Elsevier CY - Oxford AN - OPUS4-14179 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Trappe, Volker A1 - Hentschel, Manfred P. A1 - Ivers, Heinz ED - Gdoutos, E. T1 - Determination of inter-fibre-failure in complex, reinforced composites T2 - 16th European Conference of Fracture "Fracture of Nano and Engineering Materials and Structures" CY - Alexandroupolis, Greece DA - 2006-07-03 PY - 2006 SN - 1-402-04971-4 IS - 900_tra SP - 1 EP - 8(?) PB - Springer CY - Dordrecht AN - OPUS4-14183 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Grasse, Fabian A1 - Meister, O. T1 - Lifetime enhancement for GFRP-gliders using a representative substructure T2 - International Conference on Fatigue of Composites (ICFC 4) CY - Kaiserslautern, Germany DA - 2007-09-26 PY - 2007 AN - OPUS4-16387 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Werkstoffermüdung bei Compsites mit polymerer Matrix / insbesondere CFK unter Betriebsbeanspruchungen T2 - DVM / DGM-Tagung CY - Osnabrück, Germany DA - 2007-09-17 PY - 2007 AN - OPUS4-16390 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Non-invasive characterisation of interlaminar fatigue of carbon fibre composites T2 - Aero-Space-Testing-Messe 2004 CY - Hamburg, Germany DA - 2004-04-01 PY - 2004 AN - OPUS4-5881 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Charakterisierung des Schädigungsverhaltens von FVW zur Lebensdauervorhersage sicherheitsrelevanter FVW-Bauteile T2 - BAM-Kolloquium CY - Berlin, Germany DA - 2004-04-28 PY - 2004 AN - OPUS4-5882 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Lenke, Karoline A1 - Hentschel, Yvonne A1 - Trappe, Volker T1 - Multiaxially loaded short fibre polyamide: a contribution to non-destructive evaluation of micro cracking and damage evolution N2 - Short fibre reinforced thermoplastics are increasingly used in automotive applications because of their potential for light weight design and cost efficient manufacturing by injection moulding. The fibre orientation, tuneable in the production process, defines the degree of anisotropy which causes different damage behaviour depending on the multiaxial stress state. Therefore, the multiaxial damage behaviour, based on micro cracking, is analysed by combining mechanical loading tests and non-destructive X-ray refractometry. T2 - ICCM19 - 19th International conference on composite materials CY - Montreal, Canada DA - 28.07.2013 KW - Short fiber reinforced composites KW - Multiaxial loading KW - Non-destructive testing KW - X-ray refraction KW - Damage mechanics PY - 2013 N1 - Geburtsname von Lenke, Karoline: Metzkes, K. - Birth name of Lenke, Karoline: Metzkes, K. SP - 5725 EP - 5733 AN - OPUS4-29004 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Hörold, Andreas A1 - Schartel, Bernhard A1 - Trappe, Volker A1 - Korzen, Manfred A1 - Naumann, Maurice T1 - Structural integrity of sandwich structures in fire: an intermediate-scale approach N2 - A test set-up in intermediate scale was conceived to investigate the structural integrity of materials under fire. The task was to develop a realistic test scenario targeting component-like behaviour. Carbon-fibre-reinforced sandwich specimens (500 X 500 X 20 mm) were used to examine failure mechanisms, times to failure and critical failure loads under compression. Fire tests were performed with fully developed fire applied to one side of the specimen by an oil burner. In a first test series, the applied load was varied, but the fully developed fire remained unchanged. In general, times to failure were short. Decreased load levels resulted in prolonged times to failure and led to a different failure mechanism. Results obtained in the test series were compared with a bench-scale study (150 X 150 X 20 mm) investigating identical material. The comparison clearly revealed the influence of size on the time to failure and the load-bearing capacity. KW - Fire testing KW - Structural integrity KW - Carbon-fibre-reinforced plastics KW - Fully developed fire KW - Composites PY - 2013 U6 - https://doi.org/10.1080/15685543.2013.816620 SN - 0927-6440 SN - 1568-5543 VL - 20 IS - 9 (Special Issue: ECCM15: Part 3) SP - 741 EP - 759 PB - VSP CY - Zeist AN - OPUS4-29647 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Günzel, Stephan A1 - Trappe, Volker ED - Holger Frenz, ED - Grellmann, Wolfgang T1 - Ermittlung bruchmechanischer Kennwerte an Epoxid-Harzen T2 - Tagung Werkstoffprüfung 2008 "Herausforderungen neuer Werkstoffe an die Forschung und Werkstoffprüfung" CY - Berlin, Deutschland DA - 2008-12-04 KW - Rissfortschritt KW - Risszähigkeit KW - Epoxid-Harz KW - Crack growth KW - Fracture toughness KW - Epoxy resin PY - 2008 SN - 978-3-00-026399-6 SN - 1861-8154 N1 - Serientitel: DVM-Bericht – Series title: DVM-Bericht VL - 642 IS - 642 SP - 295 EP - 300 PB - DVM CY - Berlin AN - OPUS4-18778 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebszeitfeste Auslegung von FKV - Effekte, Grenzen, Möglichkeiten T2 - Fachtagung "Dimensionieren mit faserverstärkten Kunststoffen", Institut für Kunststoffverarbeitung (IKV) an der RWTH Aachen CY - Aachen, Germany DA - 2009-06-04 PY - 2009 AN - OPUS4-19166 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Praxisgerechte und effiziente Prüfung der Betriebsfestigkeit von Faserverbundwerkstoffen und -bauteilen T2 - 15. Nationales Symposium SAMPE Deutschland e. V., BAM CY - Berlin, Germany DA - 2009-02-18 PY - 2009 AN - OPUS4-19168 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Basan, Ricardo A1 - Trappe, Volker A1 - Grasse, Fabian T1 - Bestimmung der Schubeigenschaften von Faserverbundwerkstoffen mittels eines Schubrahmens T2 - Deutscher Luft- und Raumfahrtkongress 2009 CY - Aachen, Deutschland DA - 2009-09-08 KW - Faserverbundwerkstoffe KW - Schubrahmen KW - Schubeigenschaften PY - 2009 SN - 1868-8764 IS - DocumentID: 121274 SP - 1 EP - 8 AN - OPUS4-20464 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Grasse, Fabian A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Meister, O. T1 - Lifetime assessment for GFRP-gliders using a representative substructure N2 - In a research project fatigue tests on two identical wing sections that are used as representative substitute components were performed to estimate lifetime enhancement of light-weight aircraft such as general aviation gliders. Single step fatigue tests at limit load on one component were compared with spectrum loading on the other. A characteristic damage behaviour was observed. Local buckling due to high shear loading of the sandwich core of the wing shell causes the main damage. Even though an intentionally high load level was chosen no increase of micro-cracking could be detected. Additionally no delamination effects in laminates or bondings were observed except the skin-core delamination which causes the buckling effect in the wing shell due to fatigue loading. Finally the concept of using representative substructures and accompanying specimen tests is an effective approach for in-service loading investigations and could also be applied to research on wind turbine blades. KW - Glass fibre reinforced plastics (GFRP) KW - Grey scale value analysis KW - X-ray-refraction KW - Non-destructive testing (NDT) KW - Fatigue tests PY - 2010 U6 - https://doi.org/10.1016/j.ijfatigue.2009.02.003 SN - 0142-1123 VL - 32 IS - 1 SP - 94 EP - 99 PB - Elsevier CY - Oxford AN - OPUS4-20498 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Müller, Bernd R. A1 - Trappe, Volker A1 - Goebbels, Jürgen A1 - Hickmann, Stefan A1 - Grasse, Fabian T1 - Non-destructive characterization of composites: from small scale to complex component testing - a challenge T2 - International Symposium on NDT in Aerospace CY - Hamburg, Germany DA - 2010-11-22 KW - Aircraft KW - Wind turbine blades KW - Automotive KW - X-ray refraction KW - Fibre orientation KW - WAXS technique KW - X-ray computed tomography PY - 2010 SN - 978-3-940283-28-3 IS - DGZfP-BB 124 (Tu.2.B.1) SP - 1 EP - 6 AN - OPUS4-22724 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Jaunich, Matthias T1 - Correlation between crack propagation rate and cure process of epoxy resins T2 - International Conference on Fatigue of Composites (ICFC 5) CY - Nanjing, China DA - 2010-10-16 PY - 2010 AN - OPUS4-22139 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Mix, Renate T1 - Kompatibilität und Qualität von Faserhalbzeugen und Matrix-Werkstoffen - Etablierte Verfahren und neue Konzepte T2 - Symposium für Segelflugzeugentwicklung 2010 CY - Braunschweig, Germany DA - 2010-11-18 PY - 2010 AN - OPUS4-22856 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Testing of lightweight composite structures - from complex component setup to micro-mechanical analysis T2 - Vortragseinladung des Centro de Investigatión Cientifica de Yucatán CY - Mérida, Mexico DA - 2012-10-04 PY - 2012 AN - OPUS4-26692 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Goebbels, Jürgen T1 - Zerstörungsfreie Charakterisierung des Schädigungszustandes von kurzglasfaserverstärkten Thermoplasten mit Röntgenverfahren T2 - DACH-Tagung CY - Graz, Austria DA - 2012-09-16 PY - 2012 AN - OPUS4-26689 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Goebbels, Jürgen T1 - MODELLING THE DAMAGE BEHAVIOUR OF SHORT FIBRE REINFORCED COMPOSITES USING A NON-DESTRUCTIVELY EVALUATED FIBRE ORIENTATION DISTRIBUTION AND MICRO CRACKING T2 - ECCM-15 CY - Venice, Italy DA - 2012-06-24 PY - 2012 AN - OPUS4-26690 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Goebbels, Jürgen T1 - Modelling the damage behaviour of short fibre reinforced composites using a non-destructively evaluated fibre orientation distribution and micro cracking T2 - ECCM15 - 15th European conference on composite materials CY - Venice, Italy DA - 2012-06-24 KW - Short fiber reinforced plastics KW - Nondestructive testing KW - Micro cracking KW - Damage mechanics PY - 2012 SN - 978-88-88785-33-2 SP - 1 EP - 6(?) AN - OPUS4-26777 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Jaunich, Matthias T1 - Correlation between crack propagation rate and cure process of epoxy resins N2 - Fracture mechanics approaches are increasingly applied for the characterization of epoxy resin and adhesive mechanical properties. Therefore, the fracture toughness and crack resistance under static load ISO 13586 [1] are often regarded as state of the art to analyse material improvements. However, experimental investigations on fatigue behaviour, thus the crack propagation according to ISO 15850 [2], seem to be much more sensitive to characterize the materials for in service loading conditions. Firstly, an efficient testing concept was developed at BAM. In this framework, the geometry for a modified single edge notched tensile specimen (SET) was developed in order to assure appropriate resolution in measuring the crack length via a CCD-camera [3]. In the next step, the influence of the cure temperature on the fracture-mechanical properties was investigated. KW - Fracture toughness KW - Crack resistance KW - Fracture mechanics KW - Plastics KW - Crack propagation PY - 2012 U6 - https://doi.org/10.1016/j.polymertesting.2012.03.007 SN - 0142-9418 VL - 31 IS - 5 SP - 654 EP - 659 PB - Elsevier Science CY - Amsterdam [u.a.] AN - OPUS4-26937 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Günzel, Stephan A1 - Hickmann, Stefan A1 - Wittemeyer, Christian A1 - Trappe, Volker T1 - Effects of fiber orientation and moisture on the crack growth in short glass fiber reinforced polyamide N2 - Short glass fiber reinforced polyamides are increasingly used in automotive applications. Concepts and models are needed, which enable the prediction of the structural durability. The fiber orientation and the content of moisture have a major influence on the fracture mechanical properties and on the damage mechanisms. The complex crack growth behavior was investigated and described in an empirical model. PY - 2012 U6 - https://doi.org/10.1002/adem.201100337 SN - 1438-1656 VL - 14 IS - 10 SP - 867 EP - 872 PB - Wiley-VCH Verl. CY - Weinheim AN - OPUS4-26938 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Sachs, Patrick T1 - Dynamic mechanical analysis of epoxy-matrix cross linking measured in-situ using an elastomer container N2 - A new patented dynamic mechanical analysis (DMA) is presented, where the tensile, bending- or torsional stiffness of a media can be characterized in-situ during the phase transition from liquid to solid. An epoxy system, e.g. Hexion L285/H287, is filled into an elastomer container, such as a silicone tube. This can be mounted into a conventional DMA and, based on a linear viscoelastic approach, the storage modulus (E’;G’), the loss modulus (E’’;G’’) and the loss angle tan(delta) can be measured at constant temperature as a function of time in order to investigate the liquid to sol-gel to solid transition. With this new method, the stiffness increase as a result of the cure process can be directly measured more precisely than with a rheometer in a shear plate set-up, because using an elastomer container gives a defined cross section for calculating the Young’s modulus. T2 - 20th European Conference on Composite Materials, ECCM20 CY - Lausanne, Switzerland DA - 26.06.2022 KW - Dynamic mechanical analysis (DMA) KW - Thermoset polymers KW - Cure process KW - Cross linking PY - 2022 AN - OPUS4-55213 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Current and future technological advancement in polymer matrix composites enabled through fundamental discoveries N2 - This presentation is a summary of the work from the past 20 years’ development of PMC-testing at the BAM-FB 5.3 with respect to safety-relevant design of advanced light weight structures in aircraft, wind turbine and automotive applications. The talk begins with wood as an example from nature, and emphasizes that load case, fiber architectural design and the production process and quality have to go hand in hand to generate an advanced light weight structure. Since PMC-relevant basic findings of mankind span across hundreds of years, high-performance composite applications today are based more on long term experiences than on breakthrough inventions of modern days. In the second part of the talk, future plans and projects of FB-5.3 are presented, specifically addressing H2-safety, circular economy, recycling by design and digitalization of PMC-technologies. T2 - Abteilungsseminar CY - Online meeting DA - 07.09.2021 KW - Polymer Matrix Composites KW - Thermo mechanical fatigue PY - 2021 AN - OPUS4-54150 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Beschreibung des Ermüdungsverhaltens von Endlos-Faserverstärkten-Kunststoff-Verbunden mit Hilfe mikromechanischer Modelle N2 - Im Rahmen des Vortrags werden die neusten Ergebnisse aus dem Fachbereich 5.3 zur Beschreibung des Ermüdungsverhaltens von FKV mittels Mikromechanischer-Modelle präsentiert. Explizit wird der theoretische Ansatz am Beispiel von GFK unter thermomechanischer Beanspruchung hergeleitet und an Hand von Versuchsergebnissen verifiziert. T2 - Webkonferenz Composites United, Composite Fatigue CY - Online meeting DA - 30.09.2021 KW - Faser-Kunststoff-Verbunde KW - thermomechanische Beanspruchung KW - Materialmodell PY - 2021 AN - OPUS4-54151 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kraus, David T1 - Thermo-mechanical fatigue of glass fiber reinforced polymer N2 - Glass fiber reinforced polymer (GFRP) materials in practical applications have to endure cyclic mechanical loading in a wide temperature range (e.g. aircraft applications, automotive, wind turbine blades). In this study the static strength and fatigue behavior of GFRP was investigated in a temperature range from 213 K to 343 K. Therefor the coefficients of thermal expansion of the composite as well as the matrix are measured in this temperature interval. The inverse laminate theory was extended and used to calculate the inter fiber-failure effort for a virtual UD-layer according to the layer wise strength approach. The experimentally determined results are compared with the micro-mechanical model according to Krimmer, which has been enhanced to include the effect of temperature and fiber-perpendicular failure modes. A correlation between matrix effort, the dilatational strain energy of the matrix and the damage state of the specimen is demonstrated. It is shown that a fatigue life assessment can be performed with the aid of a temperature-independent master fatigue curve, as it was similar done for the fatigue behavior of CFRP and GFRP to very high load cycles at room temperature. T2 - ICFC8 - The 8th International Conference on the Fatigue of Composites CY - Online meeting DA - 23.06.2021 KW - Glass fibre reinforced plastics KW - Fatigue KW - Thermo-mechanical-loading PY - 2021 AN - OPUS4-52910 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Portella, Pedro Dolabella A1 - Trappe, Volker A1 - Trappe, Volker A1 - Nielow, Dustin T1 - Non-destructive characterization methods for polymer matrix composites N2 - The mechanical behavior of fiber reinforced composites with polymer matrix is governed by several mechanisms operating at different length scales. In this contribution we describe first non-destructive techniques which are adequate for the characterization of the fiber-matrix interphase at a microscopic level. In a second step we describe on a mesoscopic level the influence of manufacturing related elements on the mechanical properties of rotor blades for wind turbines. We concentrate on thermography, laminography and ultrasound in connection with mechanical testing systems. Finally we present methods for monitoring rotor blades by using embedded optical fibers. T2 - Universidade do Estado do Rio de Janeiro (UERJ), Nova Friburgo, RJ, Brasilien CY - Online meeting DA - 26.11.2020 KW - Polymer matrix composites PY - 2020 AN - OPUS4-52043 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Kraus, David A1 - Trappe, Volker T1 - Transverse damage in glass fiber reinforced polymer under thermo-mechanical loading N2 - In this study, the thermomechanical damage behavior of a glass fiber reinforced polymer material is investigated. The coefficients of thermal expansion of the composite as well as the matrix are measured in a wide temperature range. Quasi-static experiments with neat resin, unidirectional and multidirectional laminates are performed as well as fatigue experiments in a temperature range from 213 K to 343 K. This study focusses on the matrix damage due to fiber-parallel loading. A correlation between matrix effort, the dilatational strain energy of the matrix and the damage state of the specimen is demonstrated. It is shown that a fatigue life assessment can be performed with the aid of a temperature-independent master fatigue curve. KW - Composite KW - Glass fiber reinforced polymer KW - Thermo-mechanics KW - Fatigue KW - Damage KW - Temperature PY - 2021 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-527462 SN - 2666-6820 VL - 5 SP - 100147 PB - Elsevier B.V. AN - OPUS4-52746 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Schartel, Bernhard A1 - Timme, Sebastian A1 - Hörold, Andreas A1 - Trappe, Volker A1 - Korzen, Manfred T1 - Composites in fire: Intermediate-scale testing of sandwich panels and shells N2 - Intermediate-scale testing is indispensable when investigating the fire resistance under simultaneous compressive load of components made of glass- and carbon-fibre-reinforced composites (GFRP and CFRP). BAM is successfully operating an intermediate-scale test stand, developed for a specimen size of 500 mm x 500 mm (1000 mm). The fire resistance in terms of fire stability of CFRP and GFRP sandwiches are investigated, e.g. at 20 % of their compressive failure load at room temperature. Times to failure increase by up to a factor of 4 due to intumescent coatings. For GFRP sandwiches, different core structures with and without additional flame retardants show an astonishing impact on time to failure. CFRP shell structures are investigated on the intermediate scale with and without stringer reinforcements, resulting in completely different mechanical failure behaviour in the ultimate load test as opposed to the fire resistance test. The stringers become the only load-carrying part, while the shell acts as a protective layer. Thus the design exploiting this self-protection potential, i.e. the residue of the front skin protecting the load-bearing structure, is highlighted as a most promising route to enhance the fire resistance of lightweight materials. T2 - Interflam 2016 CY - Egham, Surrey, UK DA - 04.06.2016 KW - composite KW - fire stability KW - fire resistance KW - sandwich panels KW - shells KW - intermediate-scale testing PY - 2016 SN - 978-0-9933933-2-7 SN - 978-0-9933933-3-4 VL - 2 SP - 1465 EP - 1470 PB - Interscience communications AN - OPUS4-36892 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Basan, Ricardo A1 - Grasse, Fabian T1 - STIFFNESS AND FRACTURE OF SHEAR LOADED LAMINATES WITH UNIDIRECTIONAL AND BIAXIAL FIBRE ORIENTATION INVESTIGATED WITH A PICTURE FRAME TEST T2 - The 16th European Conference on Composite Materials (ECCM16) CY - Sevilla, Spain DA - 2014-06-22 PY - 2014 AN - OPUS4-32096 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Ortwein, Hans-Peter A1 - Hickmann, Stefan T1 - Infinite life of CFRP evaluated nondestructively with X-ray-refraction topography N2 - CFRP are more and more used in modern civil aircrafts hence the whole fuselage is made of this material (B787; A350). Due to strict certification Standards finally the normal in-service loading gives a low stress level compared to the static and even the fatigue strength of the material. Hence CFRP are assumed to have an infinite life. To evaluate this assumption, fatigue tests on CFRP-specimens were performed up to 108 load cycles. The first inter-fiber failure was evaluated non-destructively by the fatigue tests accompanying X-ray-refraction topography altemately and in-situ mechanical loading. The basic idea of the investigation is represented in fig. 1. At low load levels it could not be assumed the total failure of the samples. Hence accompanying non-destructive testing (NDT) is mandatory to get information about the damage state of the material. T2 - ICCM19 - 19th International conference on composite materials CY - Montreal, Canada DA - 28.07.2013 KW - Carbon fibre reinforced plastics (CFRP) KW - Very high cycle fatigue (VHCF) KW - Non-destructive testing (NDT) KW - X-ray refraction KW - Damage mechanics PY - 2013 SP - 1 EP - 8 AN - OPUS4-31169 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Lenke, Karoline A1 - Trappe, Volker T1 - Damage evolution in short fibre reinforced polyamide caused by biaxial loading N2 - The multiaxial fatigue damage behaviour of short fibre reinforced polyamide 6 is analysed on injection moulded tube samples. In parallel with the fatigue tests, the damage state is evaluated nondestructively by X-ray refraction analysis which detects inner surfaces by the variation of electron density. By applying X-ray refraction analysis and a model based on by GÜNZEL the micro damage evolution can be separated into fibre matrix debonding and matrix-Micro cracking. T2 - ECCM16 - 16th European conference on composite materials CY - Seville, Spain DA - 22.06.2014 KW - Short fibre reinforced composites KW - Multiaxial loading KW - Non-destructive testing KW - Damage evolution KW - Damage state PY - 2014 SN - 978-84-616-9798-4 N1 - Geburtsname von Lenke, Karoline: Metzkes, K. - Birth name of Lenke, Karoline: Metzkes, K. SP - 1 EP - 8 AN - OPUS4-31042 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Zerstörungsfreie Prüfung von Faser-Kunststoff-Verbunden mit Röntgenstrahlen - Struktur-Eigenschafts-Beziehungen, Auflösung, technische Relevanz T2 - Einladung zum Kolloquium des IZFP Saarbrücken CY - Saarbrücken, Germany DA - 2013-12-02 PY - 2013 AN - OPUS4-31109 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Lenke, Karoline A1 - Ortwein, Hans-Peter A1 - Hickmann, Stefan T1 - Mikrorissbildung in Faser-Kunststoff-Verbunden charakterisiert mit SAXS - Materialforschung und Praxis T2 - Symposium Zerstörungsfreie-Materialcharakterisierung CY - Berlin, Germany DA - 2013-11-19 PY - 2013 N1 - Geburtsname von Lenke, Karoline: Metzkes, K. - Birth name of Lenke, Karoline: Metzkes, K. AN - OPUS4-31110 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebszeitfeste Auslegung von FVK Effekte, Grenzen und Möglichkeiten der Lebensdauerberechnung von FVK T2 - IKV-Fachtagung "Dimensionieren mit faserverstärkten Kunststoffen" CY - Aachen, Germany DA - 2013-09-26 PY - 2013 AN - OPUS4-31111 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Ortwein, Hans-Peter A1 - Hickmann, Stefan T1 - INFINITE LIFE OF CFRP EVALUATED NONDESTRUCTIVELY WITH X-RAY-REFRACTION TOPOGRAPHY T2 - The 19th International Conference on Composite Materials (ICCM) CY - Montreal, Canada DA - 2013-07-28 PY - 2013 AN - OPUS4-31112 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Grasse, Fabian A1 - Basan, Ricardo T1 - Zustandsüberwachung von Rotorblättern T2 - Vortragseinladung auf der Fachtagung "Rotorblätter von Windenergieanlagen" CY - Essen, Germany DA - 2010-06-14 PY - 2010 AN - OPUS4-21483 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Praxisgerechte und effiziente Prüfung der Betriebsfestigkeit von Faserverbundwerkstoffen und -bauteilen T2 - Kolloquium der Fraunhofer-Einrichtung für Polymermaterialien und Composite (PYCO) CY - Teltow, Germany DA - 2009-04-28 PY - 2009 AN - OPUS4-19163 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Zustandsüberwachung von Rotorblättern T2 - Fachtagung "Rotorblätter von Windenergieanlagen", Haus der Technik CY - Essen, Germany DA - 2009-06-23 PY - 2009 AN - OPUS4-19164 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker A1 - Günzel, Stephan T1 - Characterization of crack propagation in epoxy resins and adhesives PY - 2009 SN - 1619-2486 VL - 11 SP - 152 EP - 155 PB - ddp Goldenbogen CY - Dresden AN - OPUS4-20603 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Hickmann, Stefan T1 - Non-destructive evaluation of micro cracking in short fibre reinforced thermoplastics with X-ray-refraction T2 - 17th International Conference on Composite Materials (ICCM) CY - Edinburgh, Scotland DA - 2009-07-26 PY - 2009 AN - OPUS4-20538 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Rücker, Werner A1 - Rohrmann, Rolf A1 - Fritzen, C.-P. A1 - Trappe, Volker A1 - Habel, Wolfgang T1 - Results and experiences from the research project IMO-WIND N2 - Following a modular concept an integrated monitoring system has been developed that includes all components of offshore wind turbines (OWEC). Using commercially available measurement equipments of the involved partners this system was tested at the wind turbine Multibrid M5000_2 in Bremerhaven. Additional results of the research project are findings on the use of embedded FBG sensors in rotor blades that allow condition assessments based on local information. Newly developed algorithms for the identification of external loads and damage characteristics of the structural components have been tested in operation. Developed methods for monitoring based structural assessment were used, which will be suitable to optimize structural maintenance works. T2 - DEWEK 2010 - 10th German wind energy conference CY - Bremen, Germany DA - 2010-11-17 KW - Offshore wind turbines KW - Integrated monitoring system KW - Data management KW - Design verification KW - Structural assessment KW - Limit values KW - Load identification KW - Data analysis KW - Damage identification KW - Rotor blades KW - Embedded sensors PY - 2010 IS - P11.8 SP - 1 EP - 4 PB - DEWI GmbH AN - OPUS4-23714 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Basan, Ricardo A1 - Grasse, Fabian ED - Paris, Federico T1 - Stiffness and fracture of shear loaded laminates with unidirectional and biaxial fibre orientation investigated with a picture frame test N2 - Fibre Reinforced Plastics (e.g. CFRP, GFRP) characteristically show nonlinear stress-strain behaviour due to intralaminar shear loading. The determination of the in-plane shear stiffness and strength for this class of material is difficult and common test standards and methods of analysis are partially inaccurate. The identification of the in-plane shear properties was made with an especial designed “picture frame test device” which enables shear loading up to 950N/mm. Therefore the strength limit can be reached at specimens with adequate thickness and a high safety factor against buckling. Due to the chosen design the maximum of the shear loading and the final failure occur in the centre of the specimen. The experiments match with the numerical analysis. T2 - ECCM16 - 16TH EUROPEAN CONFERENCE ON COMPOSITE MATERIALS CY - Seville, Spain DA - 22.06.2014 KW - Picture frame test KW - Fibre reinforced plastics (FRP) KW - Shear strength and stiffness KW - In-situ effect PY - 2014 SN - 978-84-616-9798-4 VL - 2014 SP - ID0263 - 1 EP - 8 PB - ECCM CY - Sevilla AN - OPUS4-37617 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Müller, Alexander A1 - Nielow, Dustin A1 - Braun, Ulrike A1 - Altmann, Corinna T1 - Dauerfestigkeitsgrenze in Faser-Kunststoff-Verbunden – Einfluss der Halbzeuge N2 - Mit Hilfe der an der BAM entwickelten Röntgenrefraktionstopographie lassen sich zerstörungsfrei innere Oberflächen insbesondere in CFK messen. Somit gelingt es quantitativ und ortsaufgelöst Mikrorisse im μm-Maßstab (Faser-Matrix-Ablösungen, Matrix-Matrix-Brüche) auch im komplexen Laminat zu bestimmen. Ziel ist es, die Mikrorissbildung an Geweben und Gelegen in-situ zur Schwingbeanspruchung zu ermitteln, um Materialkonstanten und Modelle zu bestimmen, mit Hilfe derer die Zwischenfaserbruchanstrengungen angeben werden kann, bei der die Grenze zum „unendlichen“ Leben liegt, also der Werkstoff als „dauerfest“ bezeichnet werden kann. Die Schädigungsmechanismen konnten aber auch an Schalenstrukturen aus GFK mit optischen Verfahren und mit In-Situ-Messungen mittels Thermographie nachgewiesen werden. Zudem spielt die Faser-Matrix-Grenzfläche, also die Oberflächenchemie auf der Faser sowie der Vernetzungsgrad der Epoxidharzmatrix eine entscheidende Rolle. T2 - CCeV - AG Strukturelle Integrität und UAG Composites Fatigue CY - Manching, Germany DA - 01.06.2016 KW - Faser-Kunststoff-Verbunde KW - Betriebsfestigkeit KW - Dauerfestigkeitsgrenze KW - Schädigungsmechanismen PY - 2016 AN - OPUS4-37566 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Müller, Alexander T1 - Infinite life of CFRP evaluated non-destructively with X-ray-refraction topography in-situ mechanical loading N2 - Carbon Fibre Reinforced Plastics (CFRP) are more and more used in modern civil aircrafts. These days the whole fuselage is made of this material (B787; A350). Due to strict certification standards the normal in-service loading gives a low stress level compared to the static and even the fatigue strength of the material. Hence CFRP are assumed to have an infinite life. To evaluate this assumption, fatigue tests on CFRP-specimens were performed up to 108 load cycles and the first inter-fibre failure was evaluated non-destructively by accompanying X-ray-refraction topography. A tensile testing machine was integrated in a small angle X-ray scattering (SAXS) setup. X-ray refraction topography was performed while the CFRP-samples were tensile loaded. This non-destructive technique enables the detection of micro-cracking and inter-fibre failure especially for CFRP. For Glass Fibre Reinforced Plastic (GFRP) X-ray refraction and in-situ loading has already been successfully used. The increase of inner surfaces due to inter fibre failure was measured as a function of the stress state. Fatigue tests were performed at and below the limit of inter-fibre failure strength. State of the art is to assume the failure of the samples under cyclic loading as the fatigue life. Accompanying non-destructive X-ray refraction measurements reflects the damage state and enables to trace its evolution even if the total failure of the specimens does not occur. This investigation technique is of high interest to give the engineer a design value of infinite life which is practically often reached due to knock down factors of certification standards. Finally the infinite life was found for cyclic fatigue loaded CFRP-samples even under high inter fibre transverse and shear loading investigated up to 108 load cycles. T2 - 19th World Conference on Non-Destructive Testing CY - Munich, Germany DA - 13.06.2016 KW - CFRP KW - NDT KW - Fatigue KW - Damage evolution PY - 2016 AN - OPUS4-37567 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan T1 - Stiffness and fracture of shear loaded laminates investigated with a shear frame test N2 - Fibre Reinforced Plastics (e.g. CFRP, GFRP) characteristically show nonlinear stress-strain behaviour due to intralaminar shear loading. The determination of the in-plane shear stiffness and strength for this class of material is difficult and common test standards and methods of analysis are partially inaccurate. The identification of the in-plane shear properties was made with an especial designed “picture frame test device” which enables shear loading up to 950N/mm. Therefore the strength limit can be reached at specimens with adequate thickness and a high safety factor against buckling. Due to the chosen design the maximum of the shear loading and the final failure occur in the centre of the specimen. The experiments match with the numerical analysis. T2 - ISO/TC61 CY - Berlin, Germany DA - 19.09.2016 KW - Picture frame test KW - Fibre reinforced plastics (FRP) KW - Shear strength and stiffness KW - In-situ effect PY - 2016 AN - OPUS4-37564 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kupsch, Andreas A1 - Müller, Ralf A1 - Hickmann, Stefan A1 - Müller, Alexander T1 - Dauerfestigkeitsgrenze in CFK charakterisiert mit der Röntgenrefraktionstopographie T2 - Fachausschusssitzung Materialcharakterisierung der DGZfP CY - Berlin DA - 2015-11-12 PY - 2015 AN - OPUS4-34914 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Lenke, Karoline A1 - Günzel, Stephan T1 - Ermittlung der Degradationsmechanismen in kurzfaserverstärktem Polyamid unter einachsiger Ermüdungsbelastung mittels ZfP T2 - IKV-Seminar Lebensdauerberechnung von Kunststoffbauteilen CY - Aachen, Deutschland DA - 2015-11-17 PY - 2015 AN - OPUS4-34915 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, Dustin A1 - Timme, Sebastian T1 - Faserkunststoffverbunde für moderne Leichtbauanwendungen auf dem Prüfstand T2 - Kolloquium der Chemiefreunde Erkner CY - Berlin, Deutschland DA - 2015-11-18 PY - 2015 AN - OPUS4-34916 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Lenke, Karoline T1 - Schädigungsprozesse und Betriebsfestigkeit Kurzfaser-verstärkter Thermoplaste unter mechanischer Beanspruchung. T2 - Alterung von Polymerwerkstoffen, HDT 2014 CY - München, Deutschland DA - 2014-02-26 PY - 2014 N1 - Geburtsname von Lenke, Karoline: Metzkes, K. - Birth name of Lenke, Karoline: Metzkes, K. AN - OPUS4-32145 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Grasse, Fabian A1 - Zur, Malte A1 - Trappe, Volker T1 - Schubversuch mittels Schubrahmen N2 - Für die Schubkennwertermittlung an faserverstärkten Kunststoffen existieren verschiedene Verfahren, die nur eine Prüfung bis zu einer vorgegebenen maximalen Schubdehnung zulassen. Die Grasse Zur Ingenieurgesellschaft hat auf Basis eines an der BAM entwickelten Schubrahmens ein Schubprüfsystem etabliert, das diese Nachteile aufhebt. Damit ist es nun erstmals möglich, Schubkennwerte ohne Einschränkung einer maximalen Schubdehnung effizient und mit sehr guter Reproduzierbarkeit zu ermitteln. KW - Faser-Kunststoff-Verbunde KW - Schubrahmen KW - Schubfestigkeit PY - 2014 SN - 0720-1214 SN - 0033-5126 VL - 59 IS - 10 SP - 38 EP - 41 PB - Hanser CY - München AN - OPUS4-32150 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebsfestigkeit von FKV-Werkstoffen - Effekte und Konzepte mit Proben-, Komponenten- und Stellvertreterversuchen T2 - 5. VDI Fachkonferenz Rotorblätter von Windenergieanlagen CY - Bremen, Deutschland DA - 2015-04-21 PY - 2015 AN - OPUS4-33068 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Dümichen, Erik A1 - Javdanitehran, M. A1 - Erdmann, Maren A1 - Trappe, Volker A1 - Sturm, Heinz A1 - Braun, Ulrike A1 - Ziegmann, G. T1 - Analyzing the network formation and curing kinetics of epoxy resins by in situ near-infrared measurements with variable heating rates N2 - Near-infrared spectroscopy (NIR) turned out to be well suited for analyzing the degree of cure for epoxy systems. In contrast to dynamic scanning calorimetry (DSC), where the released heat of reaction determines the degree of epoxy conversion indirectly, NIR spectroscopy is able to determine the conversion directly by analyzing structural changes. Therefore, a new heatable NIR cell was equipped with an integrated thermocouple, which enables the real sample temperature to be controlled and monitored in situ during epoxy curing. Dynamic scans at different heating rates were used for kinetic modelling, to define kinetic parameters and to predict real curing processes. The kinetic models and their parameters were validated with an isothermal and a more complex multi-step curing scenario. Two available commercial epoxy systems based on DGEBA were used with an anhydride and with an amine hardener. NIR results were compared with DSC data. The simulated conversion predicted with a model fitted on the basis of NIR and DSC dynamic scans showed good agreement with the conversion measured in the isothermal curing validation test. Due to the proven reliability of NIR in measuring the reaction progress of curing, it can be considered a versatile measurement system for in situ monitoring of component production in the automotive, aerospace and wind energy sectors. KW - Epoxy resins KW - Curing kinetics KW - Near-infrared spectroscopy KW - DSC PY - 2015 U6 - https://doi.org/10.1016/j.tca.2015.08.008 SN - 0040-6031 SN - 1872-762X VL - 616 SP - 49 EP - 60 PB - Elsevier CY - Amsterdam AN - OPUS4-34187 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan T1 - Normung des Schubversuchs mittels Schubrahmen - Erkenntnisse zur Formulierung einer ISO-Norm T2 - NA 054 DIN-Normenausschuss Kunststoffe (FNK) CY - Berlin, Deutschland DA - 2015-12-01 PY - 2015 AN - OPUS4-35078 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Impulsvortrag LeBeWind - Rotorblätter T2 - 1. Beiratssitzung im Themenfeld Energie CY - Berlin, Deutschland DA - 2015-12-01 PY - 2015 AN - OPUS4-35079 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kupsch, Andreas A1 - Müller, Bernd R. A1 - Hickmann, Stefan T1 - Dauerfestigkeitsgrenze von CFK charakterisiert mit Röntgenrefraktionstopographie in situ mechanischer Beanspruchung T2 - DGZfP / DACH Jahrestagung 2015 CY - Salzburg, Österreich DA - 2015-05-10 PY - 2015 AN - OPUS4-33184 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Betriebsfestigkeit von FKV-Werkstoffen - eine skalenübergreifende Betrachtung T2 - Forschungskolloquium "Plasma-Wind" CY - Göttingen, Deutschland DA - 2015-03-05 PY - 2015 AN - OPUS4-32717 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Lenke, Karoline A1 - Trappe, Volker T1 - Short fibre polymide under combined shear and tensile loading: a non-destructive evaluation of micro damage evolution N2 - The following paper focuses on the evolution of micro damage in short fibre reinforced polyamide. Therefore, tube samples are subjected to uni- and biaxial fatigue loadings. The evolution of micro damage is analysed by the non-destructive method of X-ray refraction analysis with consideration of the fibre orientation distribution. For validation of the applied micro damage models, fractographic analyses are performed. Concluding some general results, it has been observed that the load ratio influences the quantitative dominance of micro damage, whereas occuring damage phenomena depend on the type of loading (i.e. tension and torsion). Thus, zones in the Haigh-diagram are detected, where the occurence of damage mechanisms qualitatively and quantitatively changes. This is a basis for further research regarding anisotropic damage criteria. T2 - ICCM20 - 20th International conference on composite materials CY - Copenhagen, Denmark DA - 2015-07-19 KW - Short fibre composites KW - Fatigue KW - Damage evolution KW - Biaxial loading KW - Non-destructive testing PY - 2015 SN - 978-1629931999 SP - 1 EP - 10(?) AN - OPUS4-33799 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Lenke, Karoline A1 - Trappe, Volker T1 - Short fibre polyamide under combined shear and tensile loading: A non-destructive evaluation of micro damage evolution N2 - The following paper focuses on the evolution of micro damage in short fibre reinforced polyamide. Therefore, tube samples are subjected to uni- and biaxial fatigue loadings. The evolution of micro damage is analysed by the non-destructive method of X-ray refraction analysis with consideration of the fibre orientation distribution. For validation of the applied micro damage models, fractographic analyses are performed. Concluding some general results, it has been observed that the load ratio influences the quantitative dominance of micro damage, whereas occurring damage phenomena depend on the type of loading (i.e. tension and torsion). Thus, zones in the Haigh-diagram are detected, where the occurrence of damage mechanisms qualitatively and quantitatively changes. This is a basis for further research regarding anisotropic damage criteria. T2 - International Conference on Composite Materials ICCM20 CY - Copenhagen, Denmark DA - 19.07.2015 PY - 2015 AN - OPUS4-33825 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Hörold, Andreas A1 - Schartel, Bernhard A1 - Trappe, Volker A1 - Korzen, Manfred A1 - Bünker, J. T1 - Fire stability of glass-fibre sandwich panels: The influence of core materials and flame retardants N2 - Fire resistance has become a key property for structural lightweight sandwich components in aviation, shipping, railway vehicles, and construction. The development of future composite materials and components demands adequate test procedures for simultaneous application of compression and fully developed fire. Therefore an intermediate-scale approach (specimen size = 500 mm x 500 mm) is applied with compressive loads (up to 1 MN) and direct application of a burner to one side of the specimens, as established in aviation for severe burn-through tests. The influence of different core structures (polyvinylchloride foam, polyisocyanorate foam reinforced by stitched glass bridges, and balsa wood) was investigated for glass-fibre-reinforced sandwich specimens with and without flame retardants applied on the fabrics, in the matrix, and on surface for each specimen at the same time. Times to failure were increased up to a factor of 4. The intumescent coating prolongs the time to failure significantly. What is more, using the intrinsic potential of the front skin together with the core to protect a load bearing back skin in sandwich panels, the design of the core – here using the wood core – is the most promising approach. KW - Fire resistance KW - Fire stability KW - Glass-fibre-reinforced plastics KW - Composite KW - Core materials PY - 2017 U6 - https://doi.org/10.1016/j.compstruct.2016.11.027 SN - 0263-8223 SN - 1879-1085 VL - 160 SP - 1310 EP - 1318 PB - Elsevier AN - OPUS4-38622 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stefan A1 - Metzkes, Karoline T1 - Degradation mechanism of short-fibre reinforced polyamide due to unaxial fatigue loading evaluated by non-destructive testing and fractography N2 - The damage process of short glass fibre (30% weight) reinforced polyamide caused by mechanical loading was investigated from the beginning on micro cracking level to the incipient crack of mm-dimension. Based on high resolution computer tomography and the X-ray-refraction technique the inner surface due to micro-cracking at the short fibre ends and the fibre matrix debonding of the skin surface of the filament was determined quantitatively. With the knowledge of the fatigue crack propagation rate and fracture toughness of the material from former research projects, it was derived that the total inner surface due to micro cracks measured by X-ray refraction is much higher than the specimen could have withstand the load, supposed the surface is in a localized crack. Hence, the damage process could be described from micro to macro level. Accompanying fractographic investigations endorse the modelling based on the NDT-techniques. T2 - International Conference of Fatigue of Composites ICFC 6 CY - Paris, France DA - 25.03.2015 KW - Damage evolution KW - Fracture mechanics KW - Crack propagation KW - PA-GF30 KW - X-ray-refraction KW - Fractography PY - 2015 AN - OPUS4-38778 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, Stephan A1 - Metzkes, Karoline ED - Renard, Jacques T1 - Degradation mechanism of short-fibre reinforced PA due to uniaxial fatigue loading evaluated by NDT and fractography N2 - The damage process of short glass fibre (30% weight) reinforced polyamide caused by mechanical loading was investigated from the beginning on micro cracking level to the incipient crack of mm-dimension. Based on high resolution computer tomography and the X-ray-refraction technique the inner surface due to micro-cracking at the short fibre ends and the fibre matrix debonding of the skin surface of the filament was determined quantitatively. With the knowledge of the fatigue crack propagation rate and fracture toughness of the material from former research projects, it was derived that the total inner surface due to micro cracks measured by X-ray refraction is much higher than the specimen could have withstand the load, supposed the surface is in a localized crack. Hence, the damage process could be described from micro to macro level. Accompanying fractographic investigations endorse the modelling based on the NDT-techniques. T2 - 6th International Conference on Fatigue of Composites - ICFC 6 CY - Paris, France DA - 25.03.2015 KW - Damage evolution KW - Fracture mechanics KW - Crack propagation KW - Short-Fibre-Reinforced Polymadide KW - X-ray-refraction KW - Fractography PY - 2015 SP - 1 EP - 9 PB - ASTech CY - Paris AN - OPUS4-38779 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Basan, Ricardo T1 - Fatigue life evaluation of spar cap materials by four point bending test on width-tapered specimens N2 - The presented research project focuses on an effective method to evaluate the fatigue strength of thick unidirectional laminates to be applied in spar caps. Therefore, a width-tapered bending specimen was developed for a four point loading set up. Static and fatigue loading was performed with the load ratio of R=-1. The complex stress state was investigated numerically with a finite element analysis. Finally, the concept was proven experimentally on specimens made of pultruded fibre rods. The fatigue behaviour of continuous tapered width by water jet cutting was compared to discrete tapering by rod-drop. T2 - 20th International Conference on Composite Materials CY - Copenhagen, Denmark DA - 19.07.2015 KW - Fatigue KW - CFRP KW - Pultruded fibre rods KW - Spar cap design PY - 2015 AN - OPUS4-38781 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Basan, Ricardo T1 - Fatigue life evaluation of spar cap materials by four point bending test on width-tapered specimensa N2 - The presented research project focuses on an effective method to evaluate the fatigue strength of thick unidirectional laminates to be applied in spar caps. Therefore, a width-tapered bending specimen was developed for a four point loading set up. Static and fatigue loading was performed with the load ratio of R=-1. The complex stress state was investigated numerically with a finite element analysis. Finally, the concept was proven experimentally on specimens made of pultruded fibre rods. The fatigue behaviour of continuous tapered width by water jet cutting was compared to discrete tapering by rod-drop. T2 - 20th International Conference on Composite Materials CY - Copenhagen, Denmark DA - 19.07.2015 KW - Fatigue KW - Pultruded fibre rods KW - CFRP KW - Four point bending test KW - Spar cap design PY - 2015 UR - http://iccm20.org/fullpapers/file?f=WM39KAy5ME VL - 2015 SP - Paper 150701-2549 PB - ICCM20 CY - Copenhagen AN - OPUS4-38783 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Kupsch, Andreas A1 - Müller, Bernd R. A1 - Hentschel, M. P. A1 - Lange, A. A1 - Trappe, Volker A1 - Laquai, René A1 - Shashev, Yury A1 - Evsevleev, Sergei A1 - Bruno, Giovanni T1 - Progress survey of X-Ray refraction imaging techniques N2 - The most substantial innovations in radiographic imaging techniques of the last two decades aim at enhanced image contrast of weakly absorbing micro and nano structures by taking advantage of X-ray refraction effects occurring at outer and inner surfaces. The applications range from fibre reinforced plastics to biological tissues. These techniques comprise, among others, X-ray refraction topography, diffraction enhanced imaging, phase contrast imaging, Talbot-Lau grating interferometry, and refraction enhanced imaging. They all make use of selective beam deflections up to a few minutes of arc: the X-ray refraction effect. In contrast to diffraction, this type of interaction has a 100 % scattering cross section, as shown experimentally. Since X-ray refraction is very sensitive to the orientation of interfaces, it is additionally a tool to detect, e.g., fibre or pore orientation. If the detector resolution exceeds the size of (small) individual features, one detects the integral information (of inner surfaces) within the gauge volume. We describe the above-mentioned techniques, and show their experimental implementation in the lab and at a synchrotron source. We also show strategies for data processing and quantitative analysis. T2 - 19th World Conference on Non-Destructive Testing CY - Munich, Germany DA - 13.06.2016 KW - grating KW - topography KW - refraction KW - X-ray PY - 2016 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-366194 SN - 978-3-940283-78-8 VL - 2016/158 SP - We.3.B.2, 1 EP - 9 AN - OPUS4-36619 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Müller, Alexander A1 - Hickmann, Stefan T1 - Infinite life of CFRP evaluated non-destructively with X-ray-refraction topography in-situ mechanical loading N2 - Carbon Fibre Reinforced Plastics (CFRP) are more and more used in modern civil aircrafts. These days the whole fuselage is made of this material (B787; A350). Due to strict certification standards the normal in-service loading gives a low stress level compared to the static and even the fatigue strength of the material. Hence CFRP are assumed to have an infinite life. To evaluate this assumption, fatigue tests on CFRP-specimens were performed up to 108 load cycles and the first inter-fibre failure was evaluated non-destructively by accompanying Xray-refraction topography. A tensile testing machine was integrated in a small angle X-ray scattering (SAXS) setup. X-ray refraction topography was performed while the CFRP samples were tensile loaded. This non-destructive technique enables the detection of micro-cracking and inter-fibre failure especially for CFRP. For Glass Fibre Reinforced Plastic (GFRP) X-ray refraction and in-situ loading has already been successfully used. The increase of inner surfaces due to inter fibre failure was measured as a function of the stress state. Fatigue tests were performed at and below the limit of inter-fibre failure strength. State of the art is to assume the failure of the samples under cyclic loading as the fatigue life. Accompanying non-destructive X-ray refraction measurements reflects the damage state and enables to trace its evolution even if the total failure of the specimens does not occur. This investigation technique is of high interest to give the engineer a design value of infinite life which is practically often reached due to knock down factors of certification standards. Finally the infinite life was found for cyclic fatigue loaded CFRP-samples even under high inter fibre transverse and shear loading investigated up to 108 load cycles. T2 - 19th World Conference on Non-Destructive Testing CY - Munich, Germany DA - 13.06.2016 KW - CFRP KW - NDT KW - Fatigue KW - Damage evolution PY - 2016 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-375015 UR - https://www.ndt.net/?id=19360 SN - 978-3-940283-78-8 VL - 2016 SP - 1 EP - 9 PB - DGZFP CY - Berlin AN - OPUS4-37501 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Erdmann, Maren A1 - Trappe, Volker A1 - Sturm, Heinz A1 - Braun, Ulrike A1 - Dümichen, Erik T1 - Cure conversion of structural epoxies by cure state analysis and in situ cure kinetics using nondestructive NIR spectroscopy N2 - Non-isothermal heating rate kinetics was applied to two epoxy resin systems. In situ near-infrared (NIR) measurements were taken with a heatable NIR cell which allowed the cure to be monitored by characteristic absorption bands. An autocatalyzed reaction of the nth order was shown to describe the epoxy conversion curves. Differential Scanning Calorimetry (DSC) was used as a complementary method. The kinetic models developed by both NIR and DSC are in good accordance with experimental epoxy conversion in the in situ NIR setup for single and multiple cure temperature ramps. A linear calibration curve of the characteristic absorption bands of epoxy normalized to aromatic vibrations was introduced. The curing degree of structural epoxies that were cured according to an industrial temperature cure profile was determined by NIR using the calibration curve. The epoxy conversions of the structural components showed good agreement with the experimental in situ NIR. Several degrees of cure for structural specimens were evaluated by NIR and residual reaction enthalpy by DSC. We present the non-destructive NIR spectroscopy as an alternative to determine fast and non-destructive epoxy conversion, particularly suitable for high degrees of cure on structural components. KW - Epoxy resin KW - Curing kinetics KW - In situ near-infrared (NIR) spectroscopy KW - Differential scanning calorimetry (DSC) PY - 2017 UR - http://www.sciencedirect.com/science/article/pii/S0040603117300205 U6 - https://doi.org/10.1016/j.tca.2017.01.010 SN - 0040-6031 SN - 1872-762X VL - 650 SP - 8 EP - 17 PB - Elsevier B.V. AN - OPUS4-39123 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Kraus, David A1 - Trappe, Volker T1 - Cyclic fatigue behavior of glass fiber reinforced epoxy resin at ambient and elevated temperatures N2 - The fatigue behavior of ±45° glass fiber reinforced epoxy resin under cyclic mechanical and constant thermal loading is investigated in this study. Tests at three different temperature levels in the range 296 K to 343 K have been performed in order to create S-N curves for each temperature level. The specimen damage is measured in-situ using optical grayscale analysis. The characteristic damage state (CDS) is evaluated for each specimen. It is shown that the point of CDS is suitable as a failure criterion to compare the resulting S-N curves. With micromechanical formulations, the temperature-dependent matrix effort is calculated for each stress-temperature level. In terms of matrix effort, the longest fatigue life is reached at high temperatures, while, in terms of stress, the lowest fatigue life is reached at the highest temperatures. T2 - ECCM18 - 18th European conference on composite materials CY - Athens, Greece DA - 24.06.2018 KW - Composite KW - Fatigue KW - Thermomechanics KW - Residual stresses KW - Temperature PY - 2018 SP - 1 EP - 7 PB - European society for composite materials AN - OPUS4-45338 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Kupsch, Andreas A1 - Trappe, Volker A1 - Nielow, D. A1 - Schumacher, David A1 - Lange, A. A1 - Hentschel, M.P. A1 - Redmer, Bernhard A1 - Ewert, U. A1 - Bruno, Giovanni T1 - X-ray laminographic inspection of sandwich shell segments for wind turbine rotor blades N2 - 3D structural investigations are described by X-ray laminography studies of sandwich shell segments, made of a PVC foam core, covered by non-crimp fabric glass fibre composite lay-ups processed by vacuum assisted resin infusion of epoxy. The specific scope of this study is to image transversal flaws within the foam core (joints) and of single ply overlaps. Test flaws were purposely implemented in order to simulate typical failure under cyclic load. In a dedicated test rig for shell structures, the flaw evolution/propagation is monitored by thermography and optical 3D inspection of deformation. Due to the unfavourable preconditions for classical computed tomography as of large aspect ratio, the samples were investigated by coplanar translational laminography. Its limited range of observation angles of ± 45°, results in anisotropic artefacts about the normal to the sample surface, but the typical flaws are well visualized in the as-prepared state, in a state of early damage, and in the repaired state. T2 - 12th European conference on Non-Destructive Testing CY - Gothenburg, Sweden DA - 11.06.2018 KW - X-ray laminography KW - Wind turbine KW - Rotor blade PY - 2018 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-453931 SN - 978-91-639-6217-2 SP - 1 EP - 8 AN - OPUS4-45393 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Gaal, Mate A1 - Schadow, Florian A1 - Nielow, Dustin A1 - Trappe, Volker T1 - Prüfung von Rotorblattschalen mit Luftultraschall N2 - Um den sicheren Betrieb von Windkraftanlagen zu gewährleisten, werden Rotorblätter nach der Fertigung und nach Reparatur mit verschiedenen zerstörungsfreien Verfahren auf Schaden untersucht. Bei der Fertigung von Blattschalen, die in einer Sandwich-Schalenbauweise gefertigt werden, entstehen Imperfektionen, die unter Belastung zu großen Rissen führen können. Zur Prüfung von Blattschalen wird unter anderem Ultraschallprüfung in Kontakttechnik eingesetzt. Um den Wartungsaufwand von Ultraschallanlagen zu reduzieren und um manche Kompositstrukturen vor Koppelmittel zu schützen, wird die Anwendung von Luftultraschall erforscht. Insbesondere große Fortschritte gibt es im Bereich der Entwicklung neuer Wandler. In diesem Beitrag berichten wir über die Luftultraschallprüfung von Schalen für Rotorblätter. Es wurden typische Sandwichschalenstrukturen hergestellt und mit einem eigenentwickelten Schalenprüfstand unter simulierter Betriebsbeanspruchung belastet. Die in den Schalenprüfkörpern entstandenen Schäden wurden außerhalb des Prüfstandes mit Luftultraschall in Durchschallung untersucht. Es wurden fokussierende Wandler auf Basis von Ferroelektreten entwickelt und für diese Prüfungen eingesetzt. Mit zusätzlicher elektrischer Vorspannung konnte die Empfindlichkeit der Empfänger deutlich erhöht werden. Die nach dem Lastwechsel entstandenen Schäden in den Rotorblattschalen waren eindeutig zu detektieren. T2 - DGZfP-Jahrestagung CY - Leipzig, Germany DA - 07.05.2018 KW - Wandler KW - Rotorblattschalen KW - Luftultraschall KW - Ferroelektret PY - 2018 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-453066 SP - 7 PB - Deutsche Gesellschaft für zerstörungsfreie Prüfung e.V. (DGZfP) AN - OPUS4-45306 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Ghafafian, Carineh A1 - Popiela, Bartosz A1 - Nielow, Dustin A1 - Trappe, Volker T1 - Restoration of structural integrity – a comparison of various repair concepts for wind turbine rotor blade shells N2 - Localized patches are a cost- and time-effective method for repairing fiber-reinforced polymer (FRP) sandwich wind turbine rotor blade shells. To increase the understanding of their effect on the fatigue of the blades, this study examines the effect of various layup methods of localized repair patches on the structural integrity of composite sandwich structures. Manufactured with the vacuum-assisted resin infusion (VARI) process, the shell test specimens are produced as a curved structure with glass fiber reinforced polymer (GFRP) sandwiching a polyvinyl chloride (PVC) foam core. Patch repairs are then introduced with varying layup techniques, and material properties are examined with cyclic fatigue tests. The transition region between patch and parent material is studied in greater detail with finite element method (FEM) simulations, with a focus on the effect of fiber orientation mismatch. Damage onset, crack development, and eventual failure are monitored with in-situ non-destructive testing methods to develop a robust understanding of the effects of repair concepts on material stiffness and strength. T2 - SMAR 2019 - 5th International Conference on Smart Monitoring, Assessment and Rehabilitation of Civil Structures CY - Potsdam, Germany DA - 27.08.2019 KW - Lightweight materials KW - Glass fiber reinforced polymers KW - Sandwich KW - Wind turbine blades PY - 2019 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-482170 SP - 1 EP - 8 PB - German Society for Non-Destructive Testing (DGZfP e.V.) AN - OPUS4-48217 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Günzel, S. A1 - Lenke, Karoline T1 - Degradation Mechanism of Short-Fibre Reinforced Polyamide due to Uniaxial Fatigue Loading Evaluated by Non-Destructive Testing and Fractography T2 - International Conference on Fatigue of Composites ICFC 6 CY - Paris, France DA - 2015-03-25 PY - 2015 N1 - Geburtsname von Lenke, Karoline: Metzkes, K. - Birth name of Lenke, Karoline: Metzkes, K. AN - OPUS4-32959 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Effective composite testing for wind turbine blades - from specimen size to component scale T2 - 4th International Conference Advances in Rotor Blades for Wind Turbines CY - Bremen, Deutschland DA - 2015-02-24 PY - 2015 AN - OPUS4-32604 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Hörold, Andreas A1 - Schartel, Bernhard A1 - Trappe, Volker A1 - Gettwert, V. A1 - Korzen, Manfred T1 - Protecting the structural integrity of composites in fire: Intumescent coatings in the intermediate scale N2 - The fire behaviour of light-weight material used in structural applications is regarded as the main challenge to be solved for mass transportation. The task is to perform realistic experiments, including a mechanical test scenario under fully developed fires, to improve the material's reliability in structural applications. Our approach utilises an intermediate-scale test set-up (specimen size 500 × 500 mm) to apply realistic compressive loads and fully developed fires directly to one side of a carbon-fibre-reinforced sandwich composite. Three different intumescent coatings were applied to sandwich structures and compared to a bench-scale study. The results emphasise intumescent coatings as a promising method to sustain fire resistance, multiplying the time to failure. Nevertheless, the realistic intermediate-scale test using severe direct flame application underlines the extremely short failure times when the actual composite components are tested without any additional insulation. KW - Carbon-fibre-reinforced KW - Fire stability KW - High-temperature properties KW - Mechanical testing KW - Fully developed fire KW - Post-crash scenario PY - 2015 U6 - https://doi.org/10.1177/0731684415609791 SN - 0731-6844 SN - 1530-7964 VL - 34 IS - 24 SP - 2029 EP - 2044 PB - Technomic Publ. Co. CY - Westport, Conn. AN - OPUS4-35120 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, Dustin T1 - Fatigue loading of sandwich shell test specimens with simulated production imperfections and in-situ NDT N2 - A shell test bench was developed at BAM 5.3 which allows for static and fatigue testing of curved fiber-reinforced plastic (FRP) structures, during which in-situ the damage state can be non-destructively inspected by thermography and strain-field measurement techniques. Sandwich shell specimens with typical wind turbine blade manufacturing defects were designed and tested. The tested imperfections show a fairly significant reduction (up to 90%) of the shell test specimens‘ lifetime, depending on the type of imperfection. Using the in-situ NDT methods incorporated in the shell test bench, the location and cycle time of the initial defects and the damage evolution was investigated. T2 - 7. International Conference on Fatigue of Composites CY - Vicenza, Italy DA - 04.07.2018 KW - Fatigue of sandwich shell structures KW - Non-destructive testing KW - Wind turbine blades PY - 2018 AN - OPUS4-50126 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, Dustin T1 - Fatigue loading of sandwich shell test specimens with simulated production imperfections and in-situ NDT N2 - A shell test bench was developed at BAM 5.3 which allows for static and fatigue testing of curved fiber-reinforced plastic (FRP) structures, during which in-situ the damage state can be non-destructively inspected by thermography and strain-field measurement techniques. Sandwich shell specimens with typical wind turbine blade manufacturing defects were designed and tested. The tested imperfections show a fairly significant reduction (up to 90%) of the shell test specimens‘ lifetime, depending on the type of imperfection. Using the in-situ NDT methods incorporated in the shell test bench, the location and cycle time of the initial defects and the damage evolution was investigated. T2 - 7. International Conference on Fatigue of Composites CY - Vicenza, Italy DA - 04.06.2018 KW - Fatigue of sandwich shell structures KW - Non-destructive testing KW - Wind turbine blades PY - 2018 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-501275 SP - 1 EP - 7 AN - OPUS4-50127 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Faserkunststoffverbunde (FKV) in Forschung und Anwendung N2 - Der Fachbereich Mechanik der Polymerwerkstoffe befasst sich mit der Charakterisierung der mechanischen Eigenschaften und der Degradation von Polymeren und Faserverbundwerkstoffen, die in hochbeanspruchten, sicherheitsrelevanten Konstruktionen wie jenen des Flugzeugbaus, des Automobilbaus und der Windenergie-Industrie eingesetzt werden. Auch die Analyse der chemischen und physikalischen Eigenschaften von Polymeren zählt zu unserem Aufgabenbereich. Das Spektrum reicht von der statischen Festigkeit über die Betriebsfestigkeit, die Messung bruchmechanischer und viskoelastischer Parameter bis hin zur Formulierung molekularer Schädigungsmechanismen. T2 - VDI Arbeitskreis Kunststofftechnik, BAM, Unter den Eichen 87 CY - Berlin, Germany DA - 14.08.2019 KW - Faserkunststoffverbunde KW - Werkstoffprüfung KW - Normung PY - 2019 AN - OPUS4-50128 LA - mul AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Effective composite testing – from specimen size to component scale N2 - Even for the basic measurements of material data for design and engineering of composite structures there is a need to upgrade standards. With a new shear frame test rig more precise values can be obtained. With advanced methods in the research on the fatigue behaviour of FRP it was found a load level of infinite life for GFRP and CFRP. This is in the range of typical strain values of airliners and rotor blades in normal operation. Statistically the mean time between damage events on rotor blades is 6 years (Deutscher Windenergie Report 2006). Due to imperfection in the production the shell structures get cracks after a few years fare before the designed life time. A shell test rig was built at BAM for efficient research on the effects of defects in production. Test blades of ~10m are an efficient way for SHM research and evaluation of NDT-methods and blade geometry. T2 - colloquium genesis-puc CY - Rio de Janeiro, Brazil DA - 01.11.2019 KW - Polymer matrix composites KW - Nondestructive testing KW - New standards PY - 2019 AN - OPUS4-50129 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Polymer matrix composites investigated with NDT at BAM N2 - Statistically the mean time between damage events on rotor blades is 6 years (Deutscher Windenergie Report 2006). Due to imperfection in the production the shell structures get cracks after a few years fare before the designed life time. A shell test rig was built at BAM for efficient research on the effects of defects in production. In-situ and ex-situ NDT give a better understanding from degradation processes in composite materials. With advanced methods in the research on the fatigue behaviour of FRP it was found a load level of infinite life for GFRP and CFRP. This is in the range of typical strain values of airliners and rotor blades in normal operation. Due to the fibre-composite nature NDT techniques have to be suitable to a wide length scale to image micro cracking as well as bigger defects. Therefore different techniques have to be applied and developed. T2 - Colloquium Abendi CY - São Paulo, Brazil DA - 05.11.2019 KW - Polymer matrix composites KW - Non-destructive testing PY - 2019 AN - OPUS4-50130 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Fatigue life evaluation and certification according to CS22 N2 - The common fatigue life certification of aircrafts according to the certification Standards 23 and 25 follows a building block approach. Static tests at room temperature as well in humid and high temperature conditions are done on the coupon level. Additionally, a full-scale static and fatigue test must be performed on the complete airframe (minimum on the fuselage together with the wing). For each type-certificate the complete building block approach test program must be performed. Traditionally in Germany, the certification of sailplanes (Certification Standard 22) follows rather a family concept. A shared data base was created over the last 50 years based upon a large number of material testing. In addition to static tests at room temperature and hot-humid conditions, fatigue tests are also done on the coupon level. Additional static and fatigue tests were done on complex structures such as spar-beams, fuselages and full-scale wing structures. However, for each type-certificate, only static tests should be performed in full-scale. This concept is determined by the certification memorandum CM-S-006 “Composite Lightweight Aircraft” 2017. The presentation was given as an introduction to the discussion about the future expectations and developments of the EASA concerning the type-certification of lightweight aircrafts according to CS22 at the OSTIVE Sailplane Development Panel Meeting at the EASA in Cologne on the 11th of October 2019. T2 - OSTIV Sailplane Development Panel Meeting 2019, Europäische Agentur für Flugsicherheit (EASA) CY - Cologne, Germany DA - 11.10.2019 KW - Certification Standard 22 KW - EASA KW - Sailplane Development Panel KW - Fatigue Life Evaluation PY - 2019 AN - OPUS4-50147 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Trappe, Volker T1 - Fatigue life evaluation of composite wing spar cap materials N2 - An effective method for evaluating the fatigue strength of thick unidirectional composite laminates of wing spar caps has been presented here. A typical width-tapered bending specimen has been developed for a four-point loading set up. Static and fatigue loading was performed at a load ratio R = -1. The complex stress state has been investigated numerically by finite element analysis. Finally, the concept is proven experimentally on specimens made of pultruded fibre rods. The fatigue behavior of the continuously tapered width by water Jet cutting has been compared to discrete tapering via rod-drop. The new method enables a screening of material fatigue behavior caused by normal and shear loading. KW - Fatigue Testing KW - Pultruded fiber rods KW - CFRP KW - Four-point bending test KW - Spar cap design PY - 2019 U6 - https://doi.org/10.3139/120.111431 SN - 0025-5300 VL - 61 IS - 12 SP - 1135 EP - 1139 PB - Carl Hanser Verlag CY - München AN - OPUS4-50090 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Trappe, Volker A1 - Spancken, D. A1 - Zeiser, A. A1 - Kose, K. A1 - DeMonte, M. T1 - Kurzfaserverstärkte Thermoplaste - Zug-Druck-Schubprüfung mit einem Rohrprobekörper unter schwingender Beanspruchung N2 - Diese DIN SPEC legt ein Verfahren für die Prüfung von unverstärkten und partikel- und kurzfaserverstärkten Kunststoffen mittels Zug-Druck-Schubprüfung fest. Dieses Verfahren findet Anwendung zur Bestimmung der Schwingfestigkeit im Bereich von 103 bis 107 Schwingspielen und der Nachgiebigkeiten unter statischer Belastung sowie der Zugfestigkeit. Alle Beanspruchungen und berechneten Größen sind nennspannungs-basiert. Grundsätzlich besteht bei Rohrprobekörpern auch die Möglichkeit eine Beanspruchung in Längs- und in Umfangsrichtung durch Innendruck zu erzeugen. Dies wird in dieser Spezifikation nicht berücksichtigt, um die Anwendung überschaubar zu halten. Bei Rohrproben mit ausgeprägter Querschnittsverkleinerung (z. B. der Prüfkörper Typ B), entsteht eine Umfangsspannung auch aufgrund einer Zugkraft (siehe Anhang C). Die Umfangsspannung muss dann mittels FEA lokal berechnet werden. Das Verfahren gilt für rohrförmige Prüfkörper deren spezifische Form den Anforderungen der Werkstoff-prüfung und bei Kurzfaserverstärkung einer hohen Vorzugsausrichtung in Probenlängsrichtung genügen. Diese DIN SPEC gilt nicht für endlosfaserverstärkte Kunststoffe. Wegen der vollkommen unterschiedlichen Fertigungstechnologien und der zu erwartenden hohen Prüflasten, sind hier die Anforderungen an die Prüfkörpergeometrie gesondert zu betrachten. Es wird nicht zielführend sein, beide Werkstoffklassen in einer Norm zu behandeln. KW - Kurzfaser-verstärkte Thermoplaste KW - Zug-Druck-Schubprüfung KW - Betriebsfestigkeit KW - Rohrprobekörper PY - 2019 U6 - https://doi.org/10.31030/3085076 IS - DIN SPEC 16457:2019-12 SP - 1 EP - 58 PB - Beuth CY - Berlin AN - OPUS4-50092 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - GEN A1 - Müller, Alexander A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Ortwein, H.-P ED - Christ, Hans-Jürgen T1 - Investigation of the infinite life of fibre-reinforced plastics using X-ray refraction topography for the in-situ, nondestructive evaluation of micro-structural degradation processes during cyclic fatigue loading N2 - The described investigation of carbon-fibre-reinforced plastics (CFRP) documents that damage evolution can be observed by means of X-ray refractography. Comparative investigations with synchrotron technique on CFRP and grey-scale analysis on glass fibre-reinforced-plastics (GFRP) confirm these results. Moreover it was found that the fracture mechanical properties of the matrix system influence damage nucleation and propagation in the laminate during static and fatigue loads. Single-step fatigue tests were carried out on Laminates with RIM135 and LY556 matrix systems made from non-crimped fabric (NCF) or twill weave in different fibre orientations. The damage to the LY556 laminates was characterized by laminate cracks growing rapidly over the whole specimen width, whereas the damage on the RIM135 laminates was characterized by an earlier onset of micro-cracking followed by laminate cracks. The specimens were fatigued up to 108 (very high cycle fatigue (VHCF) regime) load cycles. S-N-curves of damage initiation were drawn and boundaries were identified for endurance within the VHCF regime. A phenomenology based model focusing on matrix stress was applied to reproduce the first inter-fibre failure (IFF) under static and fatigue loads. KW - Carbon fibre-reinforced-plastics KW - Fatigue KW - Damage evolution KW - X-ray refractography KW - Very high cycle fatigue PY - 2018 SN - 978-3-658-24531-3 U6 - https://doi.org/10.1007/978-3-658-24531-3 VL - 2018 SP - 417 EP - 439 PB - Springer Spektrum CY - Wiesbaden ET - 1. Auflage AN - OPUS4-50096 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Schumacher, David A1 - Ou, D. A1 - Ghafafian, Carineh A1 - Zscherpel, Uwe A1 - Trappe, Volker T1 - Wind turbine rotor blade testing by dual-energy laminography N2 - Modern wind turbine rotor blades consist of sandwich shell segments made from glass fiber reinforced polymers. During manufacturing, defects can arise which could lead to failure of the whole component under dynamic mechanical and thermal loads. Hence during operation defects can arise which, if detected, can be repaired locally and in-situ by applying repair patches instead of taking the whole rotor blade down and repair it remotely. This method is much more time and cost effective, since the shut-down time of the energy converter is limited to a minimum. These repair patches can, however, also lead to new defects if not applied optimally. Therefore, it is necessary to control the quality of the repair patches to ensure the best possible restoration of structural integrity of the component. As a rotor blade is an object with a large aspect ratio, X-ray laminography is predestined to provide 3D information of the objective volume. To enhance the amount of information gained from laminographic reconstruction, we use in this study a photon counting and energy discriminating X-ray detector and apply a material decomposition algorithm to the data. By inherently separating the incident spectra within the detection process into two distinct energy bins, the basis material decomposition can provide material resolved images. Choosing glass and epoxy resin as basis materials and numerically solving the inverse dual-energy equation system, the reconstructed laminographic datasets contain highly valuable information about the distribution of the basis materials within the structure. Furthermore, cross- artifacts arising from the limited angle of the projection data can be reduced by this method which allows to investigate structures that were hidden underneath the artefacts. T2 - International Symposium on Digital Industrial Radiology and Computed Tomography – DIR2019 CY - Fürth, Germany DA - 02.07.2019 KW - Laminography KW - Wind energy KW - Fiber reinforced polymer KW - Photon counting detector KW - Repair patch PY - 2019 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-484380 UR - https://www.dir2019.com/portals/dir2019/bb/Tu.3.A.1.pdf SN - 978-947971-06-0 SP - 1 EP - 13 AN - OPUS4-48438 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Munzke, Dorit A1 - Kraus, David A1 - Eisermann, René A1 - Kübler, Stefan A1 - Schukar, Marcus A1 - Nagel, Lukas A1 - Hickmann, Stefan A1 - Trappe, Volker T1 - Distributed fiber-optic strain sensing with millimeter spatial resolution for the structural health monitoring of multiaxial loaded GFRP tube specimens N2 - Due to their high strength-to-weight ratio and excellent fatigue resistance, glass fiber reinforced polymers (GFRP) are used as a construction material in a variety of applications including composite high-pressure gas storage vessels. Thus, an early damage detection of the composite material is of great importance. Material degradation can be determined via measuring the distributed strain profile of the GFRP structures. In this article, swept wavelength interferometry based distributed strain sensing (DSS) was applied for structural health monitoring of internal pressure loaded GFRP tube specimens. Measured strain profiles were compared to theoretical calculation considering Classical Lamination Theory. Reliable strain measurements with millimeter resolution were executed even at elongations of up to 3% in the radial direction caused by high internal pressure load. Material fatigue was localized by damaged-induced strain changes during operation, and detected already at 40% of burst pressure. KW - GFRP KW - Swept wavelength interferometry KW - Distributed fiber optic sensing KW - Material degradation KW - Structural health monitoring PY - 2019 U6 - https://doi.org/10.1016/j.polymertesting.2019.106085 SN - 0142-9418 VL - 80 SP - 106085 PB - Elsevier Ltd. AN - OPUS4-48950 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kremberg, Jan T1 - Betriebsfestigkeit von Struktur-Klebungen im Anwendungsgebiet der CS22 N2 - Moderne Segelflugzeuge sind voll-verklebte tragende FKV-Strukturen. Über die Schwingfestigkeit der Faser-Kunststoff-Verbunde (FKV) und die Lebensdauerabschätzung dieser Werkstoffklasse auf Basis verschiedener Lastspektren wurden insbesondere von Christoph Kensche verschiedenen Arbeiten durchgeführt und auch auf dem Symposium für Segelflugzeugentwicklung vorgestellt. Hingegen ist die Betriebsfestigkeit von Struktur-Klebungen im Anwendungsbereich der CS22 vergleichsweise wenig untersucht worden. Über die Jahre wurden in verschiedenen Projekten immer wieder Probleme in Struktur-Klebungen (u.a. Betriebsbelastungsversuche an Versuchs-Holmen) identifiziert, analysiert und spezielle Prüfverfahren weiter entwickelt (Projekt „Tragflügel neuer Technologie für die allgemeine Luftfahrt“, FK SIF765). Im Rahmen des LuFo-Vorhabens GeAviBoo (General Aviation Booster) wurde in zwei Arbeitspaketen das Thema erneut aufgegriffen und Betriebsbelastungsversuche an Klebproben durchgeführt. Im Rahmen des Vortrages werden die Erkenntnisse der letzten 10 Jahre aufbereitet und die neusten Ergebnisse vorgestellt. T2 - Symposium für Segelflugzeugentwicklung CY - Online meeting DA - 19.11.2020 KW - Polymer Matrix Composites KW - Betriebsfestigkeit KW - Klebung KW - General Aviation PY - 2020 AN - OPUS4-51861 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker T1 - Composite materials - focus polymer matrix composites (PMC) N2 - Lecture about polymer matrix composites as part of the first trainings event GW4SHM, properties, production, basic theory, testing. T2 - 1. Training GW4SHM-Project CY - BAM, Berlin, Germany DA - 23.11.2020 KW - Polymer matrix composites KW - Composite testing KW - NDT PY - 2020 AN - OPUS4-51868 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Kupsch, Andreas A1 - Trappe, Volker A1 - Müller, Bernd R. A1 - Bruno, Giovanni T1 - Evolution of CFRP stress cracks observed by in situ X-ray refractive imaging N2 - Modern air-liners and wind turbine rotor blades are made up primarily of fiber reinforced plastics. Failure of these materials heavily impairs the serviceability and the operational safety. Consequently, knowledge of the failure behavior under static and cyclic loads is of great interest to estimate the operational strength and to compare the performance of different materials. Ideally, the damage evolution under operational load is determined with in situ non-destructive testing techniques. Here, we report in-situ synchrotron X-ray imaging of tensile stress induced cracks in carbon fiber reinforced plastics due to inter-fiber failure. An inhouse designed compact tensile testing machine with a load range up to 15 kN was integrated into the beamline. Since conventional radiographs do not reveal sufficient contrast to distinguish cracks due to inter-fiber failure and micro cracking from fiber bundles, the Diffraction Enhanced Imaging (DEI) technique is applied in order to separate primary and scattered (refracted) radiation by means of an analyzer crystal. This technique allows fast measurements over large fields-of-view and is ideal for in-situ investigations. Imaging and the tensile test are run at the highest possible frame rate (0.7 s-1 ) and the lowest possible strain rate (5.5∙10-4 s -1 ). For 0°/90° non-crimp fabrics, the first inter-fiber cracks occur at 380 MPa (strain 0.8 %). Prior to failure at about 760 MPa (strain 2.0 %), we observe the evolution of nearly equidistant (1 mm distance) cracks running across the entire sample in the fully damaged state. KW - X-ray refraction KW - Diffraction Enhanced Imaging KW - Carbon Fiber Reinforced Plastics KW - In situ tensile test KW - Crack evolution PY - 2020 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-515060 SN - 1757-8981 SN - 1757-899X VL - 942 SP - 012035-1 EP - 012035-9 PB - IOP publishing CY - Bristol, UK AN - OPUS4-51506 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Ghafafian, Carineh A1 - Popiela, Bartosz A1 - Trappe, Volker T1 - Failure Mechanisms of GFRP Scarf Joints under Tensile Load N2 - A potential repair alternative to restoring the mechanical properties of lightweight fiberreinforced polymer (FRP) structures is to locally patch these areas with scarf joints. The effects of such repair methods on the structural integrity, however, are still largely unknown. In this paper, the mechanical property restoration, failure mechanism, and influence of fiber orientation mismatch between parent and repair materials of 1:50 scarf joints are studied on monolithic glass fiber-reinforced polymer (GFRP) specimens under tensile load. Two different parent orientations of [-45/+45]2S and [0/90]2S are exemplarily examined, and control specimens are taken as a baseline for the tensile strength and stiffness property recovery assessment. Using a layer-wise stress analysis with finite element simulations conducted with ANSYS Composite PrepPost to support the experimental investigation, the fiber orientation with respect to load direction is shown to affect the critical regions and thereby failure mechanism of the scarf joint specimens. KW - Scarf joint KW - Glass fiber reinforced polymers KW - Failure mechanisms PY - 2021 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-523952 VL - 14 IS - 7 SP - 1806 PB - MDPI CY - Basel, Switzerland AN - OPUS4-52395 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Kupsch, Andreas A1 - Müller, Bernd R. A1 - Laquai, René A1 - De Monte, M. T1 - Risse an gekerbten kurzglasfaserverstärkten Thermoplasten zerstörungsfrei charakterisiert mit Röntgenverfahren N2 - Proben mit einer Mittelkerbe aus Polyamid 66 mit 35% Gewichtsan-teil an Kurzglasfaser (PA-GF35) wurden im Spritzgießverfahren hergestellt und in einem ungeschädigten und durch Schwingbeanspruch geschädigten Zustand mittels Röntgenverfahren charakterisiert. Sowohl die Faserorientierungsverteilung als auch die Riss-/Mikrorissbildung wurden mit der Röntgenrefraktionstopographie in einem SAXS-Aufbau und dem Diffraction-Enhanced-Imaging am Synchrotron (BESSY II) analysiert. Beide Verfahren spiegeln in guter Übereinstimmung die Charakteristiken dieser Werkstoffklasse in Bezug auf die Fertigungsqualität und die Schädigungsme-chanismen wider. T2 - DGZfP-Jahrestagung 2017 CY - Koblenz, Germany DA - 22.05.2017 KW - Rissfortschritt KW - Kurzfaserverstärktes Polyamid KW - Röntgenverfahren PY - 2017 AN - OPUS4-43596 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Hickmann, Stefan A1 - Kupsch, Andreas A1 - Müller, Bernd R. A1 - Laquai, René A1 - De Monte, M. T1 - Risse an gekerbten kurzglasfaserverstärkten Thermoplasten zerstörungsfrei charakterisiert mit Röntgenverfahren N2 - Proben mit einer Mittelkerbe aus Polyamid 66 mit 35% Gewichtsan-teil an Kurzglasfaser (PA-GF35) wurden im Spritzgießverfahren hergestellt und in einem ungeschädigten und durch Schwingbeanspruch geschädigten Zustand mittels Röntgenverfahren charakterisiert. Sowohl die Faserorientierungsverteilung als auch die Riss-/Mikrorissbildung wurden mit der Röntgenrefraktionstopographie in einem SAXS-Aufbau und dem Diffraction-Enhanced-Imaging am Synchrotron (BESSY II) analysiert. Beide Verfahren spiegeln in guter Übereinstimmung die Charakteristiken dieser Werkstoffklasse in Bezug auf die Fertigungsqualität und die Schädigungsme-chanismen wider. T2 - DGZfP-Jahrestagung 2017 CY - Koblenz, Germany DA - 22.05.2017 KW - Kurzfaserverstärktes Polyamid KW - Röntgenverfahren KW - Rissfortschritt PY - 2017 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-435659 UR - https://www.dgzfp.de/Dienste/Publikationen?kategorie=Berichtsb%C3%A4nde SN - 978-3-940283-85-6 VL - 2017 SP - 1 EP - 11 PB - DGZfP CY - Berlin AN - OPUS4-43565 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, Dustin T1 - Betriebsfestigkeit von imperfekten und reparierten Rotorblättern N2 - Die Betriebsbeanspruchung für Rotorblätter ist aus Messungen bekannt. Schäden an Rotorblättern treten im Betrieb meistens an der Blattschale nach 4-5Jahren, weit vor der projektierten Lebensdauer von 20 Jahren auf und führen zum Anlagenstillstand, wenn sie nicht repariert werden. Mittels eines an der BAM entwickelten FKV-Sandwich-Schalenprüfkörpern kann effizient die Betriebs-festigkeit von Imperfektionen und Reparaturstellen studiert werden. Fertigungsbedingte Imperfektionen (Lagenstöße, Schaumstöße) verkürzen die Lebensdauer ggf. erheblich und führen zu Reparaturen. Experimentell konnte gezeigt werden, dass ein(e) aus-reparierte(r) Schaden/Imperfektion die Betriebsbeanspruchung deutlich besser erträgt, als die schadhafte Struktur.Die numerische Betriebsfestigkeitsvorhersage für FKV ist Gegenstand der Forschung. Gleiches gilt für die Abschätzung der Lebensdauerverkürzung infolge bekannter Fertigungsabweichungen. T2 - OFFSHORETAGE 15.03 - 16.03.2017, CY - Heiligendamm, Germany DA - 15.03.2017, KW - Rotorblätter KW - Windenergie KW - Faser-Kunststoff-Verbunde KW - Betriebsfestigkeit KW - Reparatur PY - 2017 AN - OPUS4-39440 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Gaal, Mate A1 - Schadow, Florian A1 - Nielow, Dustin A1 - Trappe, Volker T1 - Air-coupled ultrasonic ferroelectret transducers with additional bias voltage for testing of composite structures N2 - Common air-coupled transducers for non-destructive testing consist of a piezocomposite material and several matching layers. Better acoustical matching to air is achieved by transducers based on charged cellular polypropylene (PP). This material has about hundred times lower acoustic impedance than any piezocomposite, having about the same piezoelectric coefficient. The piezoelectric properties of cellular PP are caused by the polarization of air cells. Alternatively, a ferroelectret receiver can be understood as a capacitive microphone with internal polarization creating permanent internal voltage. The sensitivity of the receiver can be increased by applying additional bias voltage. We present an ultrasonic receiver based on cellular PP including a high-voltage module providing bias voltage up to 2 kV. The application of bias voltage increased the signal by 12 to 15 dB with only 1 dB increase of the noise. This receiver was combined with a cellular PP transmitter in through transmission to inspect several test specimens consisting of glass-fiber-reinforced polymer face sheets and a porous closed-cell PVC core. These test specimens were inspected before and after load. Fatigue cracks in the porous PVC core and some fatigue damage in the face sheets were detected. These test specimens were originally developed to emulate a rotor blade segment of a wind power plant. Similar composite materials are used in lightweight aircrafts for the general aviation. The other inspected test specimen was a composite consisted of glass-fiber-reinforced polymer face sheets and a wooden core. The structure of the wooden core could be detected only with cellular PP transducers, while commercial air-coupled transducers lacked the necessary sensitivity. Measured on a 4-mm thick carbon-fiber-reinforced polymer plate, cellular PP transducers with additional bias voltage achieved a 32 dB higher signal-to-noise ratio than commercial air-coupled transducers. T2 - 10th International Symposium on NDT in Aerospace CY - Dresden, Germany DA - 26.10.2018 KW - Airborne ultrasonic testing KW - Air-coupled ultrasonic testing KW - Ferroelectret KW - Composites KW - Transducers PY - 2018 SP - 1 EP - 6 AN - OPUS4-46657 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kraus, David A1 - Kübler, Stefan A1 - Eisermann, René T1 - Multiaxial fatigue damage of glass fiber reinforced polymers N2 - Fiber reinforced polymers (FRPs) are a well established material in lightweight applications, e.g. in automotive, aerospace or wind energy. The FRP components are subjected to multiaxial mechanical as well as hygrothermal loads. Common operation temperatures are in the range of 213 K and 373 K (-60 °C and 100 °C) at a relative humidity of 10% to 90%. In spacecraft applications, the environmental conditions are even more extreme. However, the correlation between multiaxial mechanical loading and harsh environment conditions have to-date not been investigated in detail. The project aims to investigate the fatigue behavior of FRPs dependent on multiaxial mechanical loading, temperature, and humidity. Extensive experimental testing is performed on flat plate and cylindrical tube specimens, accompanied by numerical and analytical calculations. T2 - 24. Nationales SAMPE Symposium CY - Dresden, Germany DA - 06.02.2019 KW - Composite KW - Fatigue KW - Thermomechanics KW - Distributed fiber optic sensors PY - 2019 AN - OPUS4-47335 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Timme, Sebastian A1 - Trappe, Volker A1 - Korzen, Manfred A1 - Schartel, Bernhard T1 - Fire stability of carbon fiber reinforced polymer shells on the intermediate-scale N2 - The fire stability of carbon fiber reinforced polymer (CFRP) shell structures was investigated using an intermediate-scale test setup. The shell specimens are representative of typical load-bearing CFRPs in modern civil aviation. The CFRP shell specimens were exposed to a fully developed fire with direct flame impingement to one side at a heat flux of 182 kW/m2. Specimens were simultaneously loaded with constant compressive force equal to 40% of the ultimate failure load. CFRP shells and four different fire retarding configurations, using integrated protective layers, were investigated. Unprotected CFRP specimens failed after just 27 s. Specimens with integrated protective layers with low heat conductivity and high burn-through resistance showed the most promising results. An integrated titanium foil decelerated the decomposition of the epoxy matrix and increased the time to failure by 68% compared to the unprotected CFRP shell. KW - Fire stability KW - Carbon fiber reinforced polymer (CFRP) KW - Thermomechanical properties KW - Buckling KW - Fully developed fire PY - 2017 U6 - https://doi.org/10.1016/j.compstruct.2017.07.025 SN - 0263-8223 SN - 1879-1085 VL - 178 SP - 320 EP - 329 PB - Elsevier Ltd. AN - OPUS4-41283 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Eisermann, René A1 - Schukar, Marcus A1 - Nagel, Lukas A1 - Hickmann, Stefan A1 - Munzke, Dorit A1 - Trappe, Volker T1 - Characterising the material degradation of inner pressure-loaded GFRP-tube specimens using distributed strain sensing N2 - Glass-fibre-reinforced plastics (GFRP) are commonly used for the construction of pressure vessels and tanks for example in automotive and aerospace industries. Especially for pressure vessels used for the storage of natural gas or hydrogen with operation pressures up to 700 bar, an early material fatigue detection is of great interest. Measuring the distributed strain profile of GFRP structures helps to understand and detect material fatigue. In this article, we demonstrate the great potential of swept wavelength interferometry (SWI) based distributed strain sensing for the monitoring of pressure vessels made from GFRP. A resin transfer molding (RTM) process was used to manufacture GFRP-tube specimens. Commercial optical fibres with polyimid coating were glued to the surface externally in circumferential and axial direction. A cyclic load of up to 150 bar was applied to the samples using a servo-hydraulic test bench. Comparing the loaded and unloaded test conditions, we determined up to 2 % elongation in circumferential direction. We demonstrate reliable distributed strain measurements with sub-centimetre spatial resolution. By monitoring these high-resolution strain profiles, we were able to detect local material degradation that manifested itself as localized strain changes. Crucially, the material Degradation could be detected already after 75 % of dat the fatigue life before a crack appeared that led to leakage. T2 - Sensoren und Messsysteme - 19. ITG/GMA-Fachtagung CY - Nürnberg, Germany DA - 26.06.2018 KW - Distributed fibre optic sensors KW - Optical backscatter reflectometry KW - Swept wavelength interferometry (SWI) KW - Structural health monitoring (SHM) KW - Composite structures KW - Optical fibre PY - 2018 UR - https://ieeexplore.ieee.org/document/8436172/ SN - 978-3-8007-4683-5 SP - 239 EP - 242 PB - VDE VERLAG GMBH CY - Berlin AN - OPUS4-45887 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Schartel, Bernhard A1 - Humphrey, J.K. A1 - Gibson, A.G. A1 - Hörold, Andreas A1 - Trappe, Volker A1 - Gettwert, V. T1 - Assessing the structural integrity of carbon-fibre sandwich panels in fire: Bench-scale approach N2 - The fire resistance of lightweight sandwich panels (SW) with carbon fibre/epoxy skins and a poly(methacryl imide) (PMI) foam core is investigated in compression under direct application of a severe flame (heat flux=200 kW m−2). A bench-scale test procedure was used, with the sample held vertically. The epoxy decomposition temperature was quickly exceeded, with rapid flash-over and progressive core softening and decomposition. There is a change in failure mode depending on whether the load is greater or less than 50% of the unexposed failure load, or in other words if one or two skins carry the load. At high loads, failure involved both skins with a single clear linear separation across each face. There is an inflection in the failure time relationship in the ∼50% load region, corresponding to the time taken for heat to be transmitted to the rear face, along with a change in the rear skin failure mode from separation to the formation of a plastic hinge. The integrity of the carbon front face, even with the resin burnt out, and the low thermal diffusivity of the core, both play key roles in prolonging rear face integrity, something to be borne in mind for future panel design. Intumescent coatings prolong the period before failure occurs. The ratio of times to failure with and without protection is proposed as a measure of their effectiveness. Apart from insulation properties, their adhesion and stability under severe fire impact play a key role. KW - Carbon fibres KW - Sandwich KW - Structural composites KW - Fracture KW - High-temperature properties KW - Surface treatments PY - 2019 U6 - https://doi.org/10.1016/j.compositesb.2018.11.077 SN - 1359-8368 VL - 164 SP - 82 EP - 89 PB - Elsevier AN - OPUS4-46908 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, D. A1 - Hickmann, Stefan A1 - Kupsch, Andreas A1 - Gaal, Mate A1 - Redmer, Bernhard A1 - Krankenhagen, Rainer T1 - Sandwich-Schalenstrukturen in situ charakterisiert mit Thermographie und Felddehnungsmessungen N2 - An der BAM wurde ein Schalenprüfstand entwickelt, mit dem typische Sandwichschalenstrukturen unter simulierter Betriebsbeanspruchung belastet werden können. Im mechanischen Ermüdungsversuch wurden in situ die Entstehung von Schäden in Schalenprüfkörpern mit Test-Imperfektionen mittels der passiven Thermographie und Felddehnungsmessungen verfolgt. Damit konnten der Zeitpunkt, der Schadensursprung und der Schadensfortschritt zerstörungsfrei bestimmt werden. Zudem wurden vergleichend Schalenprüfkörper mit Luftultraschall und der Röntgen-Laminographie untersucht. Im Rahmen eines BMWi-Forschungsvorhabens wurden die Schädigungsmechanismen evaluiert und Empfehlungen für die Praxis der Fertigung von Rotorblättern abgeleitet. In diesem Beitrag wird sich auf die Darstellung der ZfP-Verfahren und der ZfP-Ergebnisse konzentriert. T2 - DGZfP-Jahrestagung 2018 CY - Leipzig, Germany DA - 07.05.2018 KW - Windkraft KW - Rotorblatt KW - Schalenprüfstand KW - Thermographie KW - Laminographie KW - Luftultraschall PY - 2018 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-469395 VL - 166 SP - 1 EP - 11 AN - OPUS4-46939 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Kraus, David A1 - Trappe, Volker T1 - Impact of thermal loads on the damage onset of fiber reinforced plastics N2 - In this study, quasi-static material tests on unidirectional and multi-angle glass fiber reinforced epoxy laminates at ambient temperatures from -213 K to 353 K (-60 °C to +80 °C) are performed. In addition, neat resin is investigated under tension and compression loads at different temperatures. The coefficient of thermal expansion is determined for neat resin and unidirectional reinforced specimens. The dependence of the resin’s thermomechanical properties on the ambient temperature is shown. The point of damage onset at which first cracks appear within the matrix under quasi-static loading is investigated by means of optical grey scale analysis. The correlation between damage onset and effective matrix stress at different ambient temperatures is identified. An approach for the calculation of thermomechanical loads and the prediction of the damage onset by means of inverse calculations is presented. The impact of the strain blocking effect of the matrix is considered as well as residual thermal stresses due to curing and resin shrinkage. T2 - ICCM21 - 21th International conference on composite materials CY - Xi'an, China DA - 20.08.2017 KW - Fatigue KW - Composite KW - Thermomechanics KW - Fiber reinforced plastics KW - Damage onset PY - 2017 SP - 1 EP - 12 AN - OPUS4-42075 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Baeßler, Matthias A1 - Babutzka, Martin A1 - Trappe, Volker A1 - Pittner, Andreas A1 - Krankenhagen, Rainer A1 - Kühne, Hans-Carsten T1 - Vorstellung des Aktivitätsfelds Erneuerbare Energie N2 - Auf der Beiratssitzung des TF Energie wurde das Aktivitätsfeld Erneuerbare Energien in seinem breiten Spektrum (aber selektive Auswahl) vorgestellt. T2 - Beiratssitzung TF Energie CY - BAM Berlin-Adlershof, Germany DA - 09.04.2019 KW - Erneuerbare Energien KW - Windenergie PY - 2019 AN - OPUS4-47751 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Ghafafian, Carineh A1 - Trappe, Volker ED - Vassilopoulos, A. P. ED - Michaud, V. T1 - Fully-reversed fatigue behavior of scarf joint repairs for wind turbine blade shell applications N2 - To enable a quick and cost-effective return to service for wind turbine blades, localized repairs can be executed by technicians in the field. Scarf repairs, shown to be highly efficient with a smooth load transition across angled joint walls and a restored aerodynamic profile, are the focus of this work. The failure mechanisms of these structures were examined under quasi-static tensile and fully-reversed cyclic loading. While the scarf ratio was held constant at 1:50, the repair layup was varied between large-to-small and small-to-large. The effect of the presence of resin pockets and the fiber orientation mismatch between parent and repair material on the restored strength of BIAX ±45° glass fiber reinforced polymer scarf joint structures was studied. T2 - 20th European Conference on Composite Materials CY - Lausanne, Switzerland DA - 26.06.2022 KW - Fatigue KW - Scarf repairs KW - Glass fiber reinforced polymers PY - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-569646 UR - https://infoscience.epfl.ch/record/298799 SN - 978-2-9701614-0-0 VL - Vol. 5 - Applications and structures SP - 195 EP - 201 PB - Composite Construction Laboratory (CCLab) CY - Lausanne AN - OPUS4-56964 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Sachs, Patrick ED - Vassilopoulos, A. P. ED - Michaud, V. T1 - Dynamic mechanical analysis of epoxy-matrix cross linking measured in-situ using an elastomer container N2 - A new patented dynamic mechanical analysis (DMA) is presented, where the tensile, bending- or torsional stiffness of a media can be characterized in-situ during the phase transition from liquid to solid. An epoxy system, e.g. Hexion L285/H287, is filled into an elastomer container, such as a silicone tube. This can be mounted into a conventional OMA and, based on a linear viscoelastic approach, the storage modulus (E';G'), the loss modulus (E'';G'') and the loss angle tan(δ) can be measured at constant temperature as a function of time in order to investigate the liquid to sol-gel to solid transition. With this new method, the stiffness increase as a result of the cure process can be directly measured more precisely than with a rheometer in a shear plate set-up, because using an elastomer container gives a defined cross section for calculating the Young's modulus. T2 - 20th European Conference on Composite Materials CY - Lausanne, Switzerland DA - 26.06.2022 KW - Cross linking KW - Dynamic mechanical analysis (DMA) KW - Thermoset polymers KW - Cure process PY - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-569651 UR - https://infoscience.epfl.ch/record/298799 SN - 978-2-9701614-0-0 VL - Vol. 5 - Applications and structures SP - 181 EP - 186 PB - Composite Construction Laboratory (CCLab) CY - Lausanne AN - OPUS4-56965 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Azevedo do Nascimento, A. A1 - Trappe, Volker A1 - Diniz Melo, J. D. A1 - Cysne Barbosa, A. P. T1 - Fatigue behavior of self-healing glass fiber/epoxy composites with addition of poly (ethylene-co-methacrylic acid) (EMAA) N2 - The interest in repair technologies for polymer composites has increased significantly over the last decades, due to the growing use of these materials in structural applications. In this study, poly (ethylene-co-methacrylic acid) (EMAA) was used as self-healing agent to glass fiber/epoxy composite. Materials with EMAA contents of 2 wt% and 5 wt% were manufactured using Resin Transfer Molding (RTM) and the effects of the healing agent on the properties were investigated using tensile tests and Dynamic Mechanical Analysis (DMA). Results show slight variation of properties, which was more pronounced as the content of EMAA increased. In addition, the healing efficiency was investigated through fatigue tests and the addition of higher content of EMAA increased the number of cycles to failure after the healing activation cycle. KW - Fatigue KW - Glass fiber-epoxy composites KW - Self-healing KW - Smart materials PY - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-569661 SN - 0142-9418 VL - 117 SP - 1 EP - 10 PB - Elsevier Ltd. AN - OPUS4-56966 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - JOUR A1 - Ghafafian, Carineh A1 - Trappe, Volker T1 - Prolonging structural integrity—Fatigue of scarf repairs for wind turbine blade shell applications N2 - The influence of scarf repair variables on the mechanical properties of glass fiber reinforced polymer sandwich structures is examined for the application of wind turbine blade shell repairs. Reference shell specimens are tested under fully-reversed cyclic loading to understand the fatigue behavior of the sub-component structure within a range of in-service loads, to which shell specimens with a scarf joint repair are compared. A fatiguesuperior repair material is shown to improve the fatigue behavior of the repaired structures compared to the reference specimens. In separating layup and geometry, damage development is examined on the subcomponent scale for a structural understanding of a scarf repair using in-situ digital image correlation-based strain field measurements as well as passive thermography. Within scarf repair variables, the geometry is shown to play a larger role than layup in the fatigue performance of the repaired structure. KW - Polymer–matrix composites KW - Fatigue KW - Joints/joining PY - 2023 U6 - https://doi.org/10.1016/j.compositesa.2022.107419 SN - 1359-835X VL - 167 SP - 1 EP - 11 PB - Elsevier Ltd. AN - OPUS4-56942 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Ghafafian, Carineh T1 - Scarf-joint repairs under fatigue loading investigated for sandwich shell applications N2 - Wind turbine rotor blades are produced as aerodynamic, three-dimensionally formed sandwich shell structures using mainly glass fiber reinforced plastics (GFRP). The GFRP used today have the potential to withstand the harsh operating conditions of rotor blades over the projected service life of 20 years. Premature damages that occur can be traced primarily back to design and/or manufacturing imperfections, as well as unusually high load scenarios (for instance lightning strikes, or strong winds combined with system control errors). Therefore, rotor blades have to be repaired several times (on average 2-3 times) during their projected service life. Approximately 70% of these are repairs of small- to medium-sized sandwich shells, carried out by technicians directly accessing the blade by suspended roping at the wind turbine location. The goal is to execute repairs that will last over the remaining service life, i.e. be sustainable. Within the framework of a research project carried out at BAM, Division 5.3 Polymer Matrix Composites, Department 5 for Materials Engineering, not only was the geometric shape (round vs. square in relation to the top view) varied, but also the layup of the scarf repair structure, variables that have not been studied systematically to-date. Sub-component scale sandwich shell specimens with representative repairs were used in this work in addition to coupon-scale specimens that are more commonly seen in literature. These sub-component shell specimens were tested using a unique shell test bench under loading conditions representative of wind turbine blade shell operating conditions with respect to fatigue strength. Using non-destructive testing methods (field strain measurement and thermography), damage development and distribution was monitored and analyzed in-situ. As a result, a concept was developed in which the repaired areas showed at least equivalent if not higher fatigue strength than the reference shells that were not repaired. T2 - ICFC9 - The 9th International Conference on the Fatigue of Composites CY - Vicenza, Italy DA - 21.06.2023 KW - Repair of sandwich shell structures KW - Non-destructive testing KW - Wind turbine blades PY - 2023 AN - OPUS4-57929 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Kupsch, Andreas A1 - Trappe, Volker A1 - Müller, Bernd R. A1 - Bruno, Giovanni T1 - Rissentwicklung in CFK-Laminaten nachgewiesen durch in situ Röntgen-Refraktion N2 - In Leichtbauanwendungen sind Materialien mit geringen Dichten und hohen Festigkeiten gefragt. Insbesondere Faser-Kunststoff-Verbunde (FKV) erfüllen diese Anforderungen und werden zunehmend für Strukturbauteile eingesetzt. Die Oberflächen moderner Rotorblätter von Windkraftanlagen werden aus FKV gefertigt. Das Versagen dieser Materialien hat massiven Einfluss auf die Einsatzfähigkeit der gesamten Windkraftanlage. Daher ist die Kenntnis des Versagensverhaltens dieser Komponenten unter statischer und zyklischer Belastung von großem Interesse, um die Betriebsbeanspruchung abzuschätzen. Im Idealfall wird die Schadensentwicklung unter Betriebslast mit zerstörungsfreien in-situ-Prüfverfahren ermittelt. Hier berichten wir über die Beobachtung der Rissentwicklung in Carbon-Faserverstärkten Kunststoffen (CFK) unter kontinuierlicher Zugbelastung durch in-situ Synchrotron-Röntgenrefraktionsradiographie. Eine selbst entwickelte elektromechanische Zugprüfmaschine mit einem Kraftbereich bis zu 15 kN wurde in den Strahlengang an der BAMline (BESSY II) integriert. Da in herkömmlichen (Absorptions-) Radiographien Defekte wie Zwischenfaserbrüche oder Faser-Matrix-Enthaftung keinen ausreichenden Kontrast verursachen, wird zur Kontrastanhebung die Röntgenrefraktion benutzt. Hier wird das sogenannte Diffraction Enhanced Imaging (DEI) angewandt, um Primär- und gebrochene Strahlung mit Hilfe eines Analysatorkristalls zu trennen. Diese Technik ermöglicht schnelle Messungen mit einem Gesichtsfeld von einigen Quadratmillimetern (hier: 14 mm × 7.2 mm) und ist ideal für in-situ Untersuchungen. Die Bildgebung und der Zugversuch erfolgen mit einer Bildfrequenz von 0.7 / s und einer Dehnrate von 0.00055 / s . Bei 0°/90° Fasergelegen treten die ersten Zwischenfaserrisse bei 380 MPa (Dehnung 0.8 %) auf. Vor dem Versagen bei ca. 760 MPa (Dehnung 2.0 %) beobachten wir die Ausbildung eines nahezu äquidistanten Rissmusters (Risse in ca. 1 mm Abstand), das sich im geschädigten Zustand über die gesamte Probe erstreckt. T2 - DACH-Jahrestagung 2023 CY - Friedrichshafen, Germany DA - 15.05.2023 KW - Röntgen-Refraktion KW - Synchrotronstrahlung KW - CFK KW - Rissentwicklung PY - 2023 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-576230 SN - 978-3-947971-29-9 VL - BB 180 SP - 1 EP - 8 AN - OPUS4-57623 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Cysne Barbosa, Ana Paula A1 - Azevedo do Nascimento, Allana A1 - Pavasarytė, Lina A1 - Trappe, Volker A1 - Melo, D. T1 - Effect of addition of thermoplastic self-healing agent on fracture toughness of epoxy N2 - Self-healing agents have the potential to restore mechanical properties and extend service life of composite materials. Thermoplastic healing agents have been extensively investigated for this purpose in epoxy matrix composites due to their strong adhesion to epoxy and their ability to fill in microcracks. One of the most investigated thermoplastic additives for this purpose is poly(ethylene-co-methacrylic acid) (EMAA). Despite the ability of thermoplastic healing agents to restore mechanical properties, it is important to assess how the addition of thermoplastic healing agents affect properties of the original epoxy material. In this work, EMAA was added to epoxy resin and the effect of the additive on fracture toughness of epoxy was evaluated. Results indicate that although added in low concentrations, EMAA can affect fracture toughness. T2 - 6th Brazilian Conference on Composite Materials CY - Tiradentes, Minas Gerais, Brazil DA - 14.08.2022 KW - Epoxy KW - Self-healing KW - Thermoplastic KW - Fracture PY - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:kobv:b43-572707 SN - 978-65-00-49386-3 SN - 2316-1337 SP - 219 EP - 222 AN - OPUS4-57270 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Kalinka, Gerhard A1 - Loose, Florian T1 - Carbon fibre composites exemplarily research at BAM N2 - Lightweighting as a cross-cutting technology contributes significantly to achieve the European Green Deal goals. Based on, but not limited to, advanced materials and production technologies, the demand for natural resources and CO2 emmissions are reduced by lightweighting during production, as well as use phase. Therefore, lightweighting is a crucial transformation technology assisting in decoupling economic growth from resource consumption. In this manner, lightweighting contributes significantly as a key technology of relevance for many industrial sectors such as energy, mobility, and infrastructure, towards resource efficiency, climate action and economic strength, as well as a resilient Europe. To strengthen international partnerships, addressing global issues of today at the edge of science with high performance lightweight material based on carbon fibers, an overview about the BAM expertise in carbon fiber reinforced materials is given. T2 - Meeting KCarbon CY - Berlin, Germany DA - 15.06.2023 KW - Lightweighting KW - Carbon Fibers KW - Recycling KW - Push-out Test KW - multi scale testing PY - 2023 AN - OPUS4-58094 LA - eng AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Altmann, Korinna A1 - Marzik, Julian T1 - Roving-Alterung und mechanische Eigenschaften N2 - Im statistischen Mittel steht eine Windkraftanlage (WKA) in Deutschland alle 6 Jahre wegen eines Schadens an den Rotorblättern und verursacht Kosten von 20k€-40k€ infolge Ertragsausfall und Reparaturkosten. Bei über 30.000 WKA in Deutschland verursacht dies jährlichen Kosten von 100-200 Mio. €. Zu 70% sind die Ursachen Fertigungsfehler. Diesem Themenkomplex widmet sich FB-5.3 in Kooperation mit FBs der Zerstörungsfreien Prüfung (Abt. 8) schon seit Jahren. Im aktuellen Projekt geht es um einen vorzeitigen Verschleiß der Rotorblätter infolge der Verwendung gealterter Glasfaser-Rovings. (GF). Die Entwicklung moderner Windkraftanlagen hatte in Europa seinen Ursprung in den 90er Jahren. OEMs und GF-Hersteller waren dicht beisammen. Die Globalisierung des Marktes führt heute zu einer weltweiten Verschiffung der GF in feucht-warmen Containern. Je nach Beschaffenheit (Chemie) der Schlichten (Oberflächenbehandlung) von GF können diese stark altern (Hydrolyse-Effekte) und die Festigkeit kann im Bauteil um bis zu 50% abgemindert sein. In einer Kooperation mit der Rotorblattallianz, einem Zusammenschluss der OEMs, Halbzeugherstellern und Forschungsinstituten, wurden schon vor 5 Jahren in einem Forschungsprojekt (FB-5.3; VH 5538) die chemischen Mechanismen der Alterung exemplarisch für eine Glasfaser-Roving-Type aufgeklärt. Im aktuellen Projekt (FB-5.3; VH 5304) wird ein beschleunigtes Alterungsverfahren (erhöhte Temperatur und Feuchte) am Roving im un-impregnierten Zustand entwickelt und die Festigkeit nachfolgend nach Einbettung in eine Epoxid-Harz-Matrix bestimmt. Je nach Alterungszustand zeigt sich eine Abnahme der Zwischenfaserbruchfestigkeit von bis zu 50%. Nicht alle Glasfaser-Roving-Typen zeigen diesen Effekt. Es ist gelungen für OEMs und Halbzeughersteller ein handhabbares Verfahren zur innerbetrieblichen Qualitätssicherung zu entwickeln, da die wenigsten Firmen über komplexe Analyseverfahren, wie an der BAM, verfügen. T2 - Composite United - AG Faserverbund in der Windenergie CY - Braunschweig, Germany DA - 09.05.2023 KW - Faserkunststoffverbunde KW - Windenergie KW - Alterung PY - 2023 AN - OPUS4-58409 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER - TY - CONF A1 - Trappe, Volker A1 - Nielow, Dustin A1 - Hickmann, Stefan A1 - Müller, Alexander A1 - Braun, Ulrike A1 - Altmann, Korinna T1 - Dauerfestigkeitsgrenze in Faser-Kunststoff-Verbunden – Einfluss der Halbzeuge N2 - Mit Hilfe der an der BAM entwickelten Röntgenrefraktionstopographie lassen sich zerstörungsfrei innere Oberflächen insbesondere in CFK messen. Somit gelingt es quantitativ und ortsaufgelöst Mikrorisse im μm-Maßstab (Faser-Matrix-Ablösungen, Matrix-Matrix-Brüche) auch im komplexen Laminat zu bestimmen. Ziel ist es, die Mikrorissbildung an Geweben und Gelegen in-situ zur Schwingbeanspruchung zu ermitteln, um Materialkonstanten und Modelle zu bestimmen, mit Hilfe derer die Zwischenfaserbruchanstrengungen angeben werden kann, bei der die Grenze zum „unendlichen“ Leben liegt, also der Werkstoff als „dauerfest“ bezeichnet werden kann. Die Schädigungsmechanismen konnten aber auch an Schalenstrukturen aus GFK mit optischen Verfahren und mit In-Situ-Messungen mittels Thermographie nachgewiesen werden. Zudem spielt die Faser-Matrix-Grenzfläche, also die Oberflächenchemie auf der Faser sowie der Vernetzungsgrad der Epoxidharzmatrix eine entscheidende Rolle. T2 - 8. Tagung Rotorblätter von Windkraftanlagen CY - Haus der Technik, Essen, Germany DA - 16.06.2016 KW - Faser-Kunststoff-Verbunde KW - Betriebsfestigkeit KW - Dauerfestigkeitsgrenze KW - Schädigungsmechanismen KW - Rotorblätter PY - 2016 AN - OPUS4-37569 LA - deu AD - Bundesanstalt fuer Materialforschung und -pruefung (BAM), Berlin, Germany ER -